EUROPEAN AVIATION SAFETY AGENCY

Transcription

1 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING PROCEDURES MANUAL EASA-MOPP-AC-GV-OPS-0004 GV, GV-SP (G550), GV-SP (G500) GIV-X, GIV-X (G450), GIV-X (G350) Revision 1 December 03, Gulfstream Aerospace Corporation

2 DISCLAIMER FOR MAINTENANCE / OPERATIONAL / PLACARDING PROCEDURES MANUAL (EASA-MOPP-AC-GV-OPS-0004) The technical information presented herein has been determined to be correct at time of publication. However, should a direct conflict exist between this and other official publications, e.g., Master Minimum Equipment List (MMEL), Aeroplane Flight Manuals (AFM), Maintenance Manuals, those publications take precedence. COPYRIGHT 2015 GULFSTREAM AEROSPACE CORPORATION All rights reserved, including the right to reproduce this publication. No part may be reproduced, stored in any retrieval system, or transmitted in any part or form or by any means, electronic, photocopying, microfilm, microfiche, mechanical, or otherwise, without prior written permission of Gulfstream Aerospace Corporation.

3 FRONT MATTER Table of Contents General Information Revision Log Acronyms and Abbreviations TABLE OF CONTENTS SECTION ONE LINE REPLACEABLE UNIT (LRU) COMPONENT RELIEF ATA 21 AIR CONDITIONING Cabin Altitude Indication (Overhead Panel) Cabin Differential Pressure Indicator Cabin Rate of Climb Indicator Automatic Pressurisation Control Systems Manual Pressurisation Control System Semi-Auto Pressurisation Control System Cabin Altitude Pressure Warning System Pressurisation Outflow Valve Position Indicator Cockpit Zone Temperature Control System & Cabin Zone Temperature Control Systems Cockpit/Cabin Zone Temperature Indicators (Overhead Panel) Duct Temperature Indicators (Overhead Panel) Environmental Control System (ECS) Packs Three-In-One Cabin Pneumatic Pressurisation Monitoring Instrument Air Conditioning System Pack Inlet Valves Outflow Valve System Pressure Relief Valve Cabin Pressure Indicator and Control Panel Selector Panel (Semi-Auto) Remote Filter (Pressure Relief Valve PRV) CPAM (Cabin Pressure Acquisition Module) Ram Air System PSU Fan ATA 22 AUTO FLIGHT Autothrottle Systems Performance Management Systems (SmartPerf/TOLD) Control Wheel Autopilot Disconnect Buttons Autothrottle Disconnect Buttons (on Thrust Lever Handles) Autothrottle Engage/Disengage Switches (on Thrust Lever Stem) Touch Control Steering Switches (TCS) Autopilots (Flight Guidance Computers (FGC) / Flight Directors) Yaw Damper Systems Takeoff/Go-Around (TO/GA) Buttons (on Power Lever Handles) Mach Trim Systems (GV/SP/G-IV-X only) PAGE

4 TABLE OF CONTENTS (CONTINUED) ATA 23 COMMUNICATIONS Radio Communications (VHF) Cockpit Voice Recorder (CVR) Selective Call System (SELCAL) Emergency Locator Transmitters (ELT) Crewmember Interphone System Interphone Systems Cockpit Speakers Passenger Address Systems (PA) Satellite Communication Systems Prerecorded Passenger Announcement Systems Hand Held Microphones Headsets Right Side Radio Frequency Management Unit (RFMU) (GV) Alerting System (Audio/Visual) Handset Systems High Frequency (HF) Communication Systems NAVCOM Radio (GV-SP, GIV-X) Audio Interface Units (AIUs) (GV only) Datalink System Modular Radio Cabinet (MRC) Power Supplies (GV-SP, GIV-X) Communications Management Function / CMF (GV-SP, GIV-X) Controller Pilot Datalink Communications (CPDLC) ATA 24 ELECTRICAL POWER Engine Generators APU Generator Transformer-Rectifier Units (TRUs) Main Aeroplane Battery Chargers Main Aeroplane Batteries Battery Ammeters (Overhead Panel) Battery Voltmeters Electrical Power System EICAS Displays Master Power Switch Lights (Left, Right, APU, EXT) Battery Temperature Indicating System Standby Electrical System External Power System Low Battery Power Audible Warning System (Sonalert) Ground Service Bus System

5 TABLE OF CONTENTS (CONTINUED) ATA 24 ELECTRICAL POWER (continued) Hz/60Hz AC Electrical Power Systems IRU Back Up Batteries (GV) IRU Back Up Batteries (GV-SP, GIV-X) ATA 25 EQUIPMENT/FURNISHINGS Overwater Equipment Passenger Seats Crewmember Shoulder Harnesses Observer Seat(s) Megaphones Floatation Devices "Fasten Seat Belt While Seated" Signs or Placards Storage Bin(s)/Cabin and Galley Storage Compartment/Closet Cargo Restraint System Non-Required Cabin Crew Seat(s) Galley/Cabin Waste Receptacles Access Doors/Covers Exterior Lavatory Door Ashtrays External Camera System Emergency Vision Assurance System (EVAS) Pilot Seat(s) Rudder Pedal Adjustment Cockpit Convenience Items Keyed Locks Aeroplane Ladders Baggage Compartment Shelves Crewmember Torches Holder Assemblies (Including Torch) Automatic External Defibrillator (AED) and/or Associated Equipment Emergency Medical Kit (EMK) and/or Associated Equipment First Aid Kit and/or Associated Equipment Flight Crew Sleeping Facilities Passenger Convenience Items Cabin Management System

6 TABLE OF CONTENTS (CONTINUED) ATA 26 FIRE PROTECTION Portable Fire Extinguishers Wing Overheat Warning Systems APU Fire Detection System Rear Baggage Compartment Smoke Detector Systems Lavatory Smoke Detection Systems Lavatory Fire Extinguisher Systems Galley Smoke Detection Systems Galley Fire Extinguishing Systems Engine Fire Detection Systems Flame Detectors Electronic Equipment Rack Overheat Warning System Passenger Compartment Closet Smoke Detectors Entranceway Baggage Compartment Smoke Detectors Cargo Compartment Fire Detection/Suppression Systems APU Fire Bottle ATA 27 FLIGHT CONTROLS Rudder Limit Indication System Single Rudder Indication System Automatic Ground Spoiler System Electric Elevator Trim System Control Wheel Elevator Trim Switches Flap/Stabilizer Control Channels Single Speed Brake Indication System Elevator Trim Actuator Heater Systems Aileron Trim Actuator Heater Autopilot Elevator Servos (GV-SP, GIV-X) Autopilot Pitch Trim Servos (GV-SP, GIV-X) Autopilot Aileron Servos (GV-SP, GIV-X) Autopilot Yaw Damper Servos (GV-SP, GIV-X) Stall Barrier Systems Flight Control Synoptic Display Gust Lock

7 TABLE OF CONTENTS (CONTINUED) ATA 28 FUEL Fuel Tank Temperature Systems EICAS or Standby RFMU (GV) / MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems Fuel Low Quantity Warning Systems Fuel Boost Pumps Fuel Intertank Valve Heated Fuel Return System (HFRS) (GV, GV-SP) Fuel Boost Pump Warning Systems Fuel Crossflow Valve Pressure Fueling System (Single Point Refueling) Ground Service Control Panel Automatic Fueling System Fuel Cap Chains Single Point Refueling Cap Mid Wing Ejector (MWE) System (GV, GV-SP) ATA 29 HYDRAULIC POWER Brake Accumulator Pressure Gauge (Nose Wheel Well) Auxiliary Hydraulic Pump Pressure Indicator Power Transfer Unit (PTU) Hydraulic Pressure Indication PTU Hydraulic Pump (Auto Mode) Auxiliary Hydraulic Pump (Auto Mode) Left Hydraulic System Quantity Gauge (Ground Service Control Panel - Aft Equipment Area) Right Hydraulic System Quantity Gauge (Ground Service Control Panel - Aft Equipment Area) Left Hydraulic System Quantity Indication (EICAS) Right Hydraulic System Quantity Indication (EICAS) Hydraulic Reservoir Temperature Sensors Hydraulic Reservoir Replenishing System Brake Accumulator Pressure Gauge (cockpit dial) Brake Synoptic Page Accumulator Pressure Indication

8 TABLE OF CONTENTS (CONTINUED) ATA 30 ICE AND RAIN PROTECTION Cowl Anti-Ice Pressure Indication Systems Wing Anti-Ice Systems Windshield Heat Systems Side Window Heat Systems Anti-Ice Heater Switch Lights Pitot Heaters Ice Detection Systems Cowl Anti-Ice Systems Cowl Pressure Differential Indication System Windshield Blower System Cabin Window Heat System ATA 31 INDICATING/RECORDING SYSTEM Clocks (Cockpit) Flight Data Recorder (FDR) Brake Temperature Monitoring System (BTMS) G Monitor System Electronic Checklist Data Acquisition Unit (DAU) Channels (GV) Security System Engine Cowl Open Indicating System Aeroplane Personality Modules (APM) (GV-SP, GIV-X) Plastic Guard Switch Covers Configuration Management System (GV-SP, GIV-X) InfraRed Counter Measuring System (IRCM) or Directional InfraRed Counter Measuring System (DIRCM) Quick Access Recorder (QAR) XM Weather Modular Avionics Unit (MAU) Channels (GV-SP/GIV-X)

9 TABLE OF CONTENTS (CONTINUED) ATA 32 LANDING GEAR Anti-Skid System Rudder Pedal Steering System Variable Gain Nose Wheel Steering Nose Wheel Steering Accessory Hardware (Torque Link Lanyards) Emergency Landing Gear Extension Bottle Pressure Gauge (Nose Wheelwell) Emergency Landing Gear Extension Bottle Pressure Cockpit CAS Indication (Summary Page) Blow Down Bottle (GIV-X) Blow Down Bottle (GV/GV-SP) ATA 33 LIGHTS Cockpit/Flight Deck/Flight Compartment Instrument Lighting Systems (Excluding EFIS and EICAS) Passenger Cabin Interior Illumination Systems Passenger Lighted Information Signs Position Light Bulbs Beacon Light Strobes (Anti-Collision Lights) Wing Inspection Lights Landing Lights Taxi Light System Wing Tip Taxi Light Systems Floor Proximity Emergency Escape Path Marking System Lights Pulselight System (Identification Lights) Recognition Light System Logo Light System Ramp Lights Systems Flashlight Charging Systems Aft Compartment Lights (Boiler Room) Cargo Compartment Light Pylon Mounted Exterior Baggage Loading Light Systems

10 TABLE OF CONTENTS (CONTINUED) ATA 33 LIGHTS (continued) Wheel Well Lights Exterior Emergency Evacuation Lighting System Service Door Lights Dim and Test Enunciator Channels Airstair Lights Dome Light Baggage Compartment Light Torches Wing Tip Position Light LED Element Banks Tail Position Light LED Element Banks ATA 34 NAVIGATION Directional Compass Reference Sensors Attitude Reference Sensors Standby Flight Displays Weather Radar Systems VOR/ILS Navigation Systems Marker Beacon Systems Automatic Direction Finding Systems SSR Transponder Distance Measuring Equipment (DME) Systems Standby RMI (Electro-Mechanical) Radio Altimeter Systems Long Range Navigation Systems (IRS, GPS, GNSSU and LORAN) Ground Proximity Warning Systems Lasertrak NDU (GV) Flight Management Systems (CDU and Nav Computer Only) (GV only) Navigation Management Systems Lightning Sensor Systems (LSS) Stormscope Airborne Collision Avoidance System (ACAS) Microwave Landing Systems (MLS) Symbol Generators (GV) Guidance Panel Digital Indications and Mode Select Indications

11 TABLE OF CONTENTS (CONTINUED) ATA 34 NAVIGATION (continued) Altitude Alerting System Display Units Standby Magnetic Compass System (Flux Valve) (GV) Magnetometer (GV-SP, GIV-X) Non-Stabilized Magnetic Compass Head Up Display System Airborne Flight Information System (AFIS) Slip-Skid Indicator Data Loader (GV) Data Management Unit (DMU) (GV-SP, GIV-X) Air Data Computers/Systems Integrated Avionics Computers (IACs) (GV) Bus Controllers (GV) Airshow Controller System Windshear Warning and Flight Guidance System (Reactive) Windshear Detection and Avoidance System (Predictive) Cockpit Video Monitors Heads Up Checklist Enhanced Vision System (EVS) Terrain Server Function/EGPWM Modules (GV-SP, GIV-X) Advanced Graphics Modules (AGM) (GV-SP, GIV-X) Cockpit Printer Cursor Control Devices Multifunction Control Display Units (MCDU) (GV-SP, GIV-X) Advanced Graphics Module (AGM) Databases (GV-SP, GIV-X) Charts Function (GV-SP, GIV-X) Video Function (GV-SP, GIV-X) Automatic Dependent Sueviellance-Broadcast (ADS-B) System Right Side Display Controller (GV) Right Side Display Controller (GV-SP/GIV-X) Synthetic Vision Primary Flight Display (SV PFD) Functions DDA (Digital to Distance Adapter) (GV only) GNSSU WASS (Wide Area Augmentation System or SBAS Space Based Augmentation System) Function CAS Scroll Switches

12 TABLE OF CONTENTS (CONTINUED) ATA 35 OXYGEN Passenger Oxygen System and Supply Cabin Oxygen ON Warning System Oxygen Service Panel Pressure Gauges Portable Oxygen Dispensing Units (Bottle and Mask) Oxygen Supply Warning Systems Protective Breathing Equipment (PBE) Electronic Equipment Rack Oxygen Pressure Gauges Cockpit Oxygen Pressure Indications First Aid Oxygen High Landing Field Elevation Passenger Oxygen Controller high Altitude Switch ATA 36 PNEUMATIC Bleed Air Systems Bleed Air Hot Warning Systems Isolation Valve Bleed Air System Switch Capsule Lights ATA 38 WATER/WASTE Potable Water Systems Lavatory Waste Systems (Including Wheelchair Accessible Lavatories) Lavatory Dump/Drain System Vacuum Toilet Holding Tank Indicator ATA 45 CENTRAL MAINTENANCE COMPUTER Maintenance Data Acquisition Unit (MDAU) (GV) Central Maintenance Computer (CMC) (GV-SP, GIV-X)

13 TABLE OF CONTENTS (CONTINUED) ATA 46 NEW TECHNOLOGY Electronic Flight Bag Systems (EFBs) ATA 49 AIRBORNE AUXILIARY POWER Auxiliary Power Unit (APU) APU EGT Indicators (EICAS and Overhead) APU Tachometers (EICAS and Overhead) APU "READY" Light System APU Remote Oil Quantity/Servicing System APU Oil Pressure Gauges APU Oil Temperature Gauges APU Fuel Pressure Gauges APU Start Indicator Light APU Air Load Control Valve APU External Fire Warning Alarm (Fire Warning Bell) APU Air Inlet Door System Bleed Air Augmentation Valve (GV, GV-SP) Surge Control Valve (GV, GV-SP) Ignition System Channels (GV, GV-SP) EGT Thermocouple System (GV, GV-SP) Temperature Resistance Bulb (T2) Inlet Pressure Transmitter (P2) (GV, GV-SP) RPM Speed Sensor Channels (GV, GV-SP) APU Hour Meter Oil Temperature (GV, GV-SP) Deprime Solenoid (GV, GV-SP) Oil Heater (GV, GV-SP) APU Start/Engine Cowl Interrupt System

14 TABLE OF CONTENTS (CONTINUED) ATA 52 DOORS Door Warning Light System Cargo Door Operating System Cargo Door Warning Light System Door Seal Pressure Indicator Main Entry Door Normal Operating System Main Entry Door Acoustic Curtain/Door System Lavatory Door Baggage Door Warning System Main Entry Door Warning System Internal Baggage Door Warning System Internal Pocket Doors Cabin Over Wing Exit Window Warning System ATA 71 POWERPLANT EPA Tank Ejector Pump ATA 73 ENGINE FUEL & CONTROL Fuel Flow Indication Systems Fuel Low Pressure Warning Systems (EICAS) Engine FADEC Systems (GV, GV-SP) Engine FADEC System (GIV-X) ATA 74 IGNITION Ignition Systems Ignition ON Indicator Systems ATA 77 ENGINE INDICATING HP Tachometer Indications EICAS Engine Vibration Monitor Systems Sensors Standby Engine Instruments Indicating System (RFMU) (GV) Standby Engine Instruments on Multifunction Control Display (MCDU) (GV-SP, GIV-X) Engine Vibration Monitoring System

15 TABLE OF CONTENTS (CONTINUED) ATA 78 ENGINE EXHAUST Thrust Reversers ATA 79 ENGINE OIL Low Oil Pressure Warning System Engine Oil Replenishment System Impending Oil Filter Bypass Indications Oil Quantity Indication Systems (EICAS/Ground Service Control Panel) Oil Filter Pressure Switch Fault Indications ATA 80 STARTING Engine Starting Systems Auto Start System Start Valve Position Indications Start Valve Position Indicator Lights SECTION TWO CREW ALERTING SYSTEM (CAS) MESSAGE RELIEF Statement Page CAS Messages thru 2-116

16 General Information Gulfstream has developed this manual to assist operators in development of their Maintenance, Operational, and Placarding Procedures (MOP) for the Gulfstream V aircraft. This manual is intended for use in conjunction with the Gulfstream V EASA Master Minimum Equipment List (MMEL), Revision 1, dated December 03, Operators must apply to their local regulatory office for approval of a specific MEL for their aircraft. This manual s revision number will reflect the last issued EASA approved MMEL revision number. Updates to this manual prior to the next EASA approved MMEL revision will be identified by a number and/or letter following the assigned EASA revision number, e.g., first update will be reflected as Revision 1.a. The Aircraft Discrepancy Log Sheet where all inoperative items will be noted is referred to as ADLS throughout this document. Those items marked with three asterisks (***) are optional items. Those items which are not production installed items will require the operator to develop specific maintenance, operational and placarding procedures for their installation. Users should review and become familiar with the manual. 1. Formatted manual in a table format similar to MMEL. 2. Electronically formatted in Microsoft Word for Windows 3. Corrected technical errors throughout the manual. 4. Corrected typographical errors throughout the manual. Note: Note: If errors are noted in this manual, submit a fax providing details and suggested corrections for the error to Gulfstream Technical Publications at (912) If assistance is needed regarding the MMEL, MEL or MOP implementation or usage, contact the local regulatory office.

17 NOTICE NOTICE NOTICE Any time an item in the MMEL calls for an (M) procedure to be accomplished prior to dispatch with the listed item inoperative, the definitions at the beginning of the MMEL states that these procedures are normally accomplished by maintenance personnel. However, other personnel may be qualified and authorised to perform certain functions. The ultimate responsibility for the accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the operator. In short, a properly trained flight crew member may perform an (M) procedure such as but not limited to pulling and collaring circuit breakers, changing light bulbs, changing or moving Display Units, making adjustments to seats, verifying proper operation of systems or components, swapping connectors from an inoperative unit to an operative unit, and/or closing/locking of doors if that crew member has been trained to do so. It is recommended that training records be kept at the home base of operations for personnel that have been trained to perform (M) procedures. The applicable paragraph from the MMEL for (M) and (O) are below. 10. "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by the flight crew; however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as a part of the operator's manual or MEL. 11. (M) : The use of this symbol in Column 5 indicates that an appropriate maintenance procedure must be established, published and utilized prior to the first flight undertaken following discovery of the defect and, if necessary, repeated at specified intervals during operation under the terms of the (M)MEL to maintain the required level of safety. Normally, these procedures are accomplished by maintenance personnel. However, other personnel may be qualified and authorised to perform certain functions. Note: When an item is annotated (M)/(O), the / is defined as and/or, which shows that there may be different options available in respect of the MEL procedures.

18 Extended Range (ER) Operations: As described in this MOPP and specifically in relation to the types covered herein, are those flights conducted in accordance with applicable regulations, over a route that contains a point further than 120 minutes at the approved one engine inoperative cruise speed from an adequate aerodrome.

19 Revision Dates for Gulfstream Aerospace Model GV, GV-SP (G550), GV-SP (G500) GIV-X, GIV-X (G450), GIV-X (G350) EASA MOPP: (For an explanation of changes, refer to the Gulfstream Aerospace Model GV, GV-SP (G550), GV-SP (G500) GIV-X, GIV-X (G450), GIV-X (G350) EASA MMEL Highlights of Change page.) Material Dated: Reflects Update Number: Type: January 28, 2011 Original 0 December 03, 2015 Revision 1

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21 ACRONYMS AND ABBREVIATIONS 14 CFR Title 14 Code of Federal Regulations AUX Auxiliary C Degrees Celsius (or Centigrade) BATT Battery F Degrees Fahrenheit BCN Beacon A/P Autopilot BITE Built-In Test Equipment A/T Autothrottle BKUP Backup AC Alternating Current BLD Bleed ACCUM Accumulator BOT Bottom ACFT Aircraft BPCU Bus Power Control Unit ADF Automatic Direction Finder BRK Brake ADI Attitude Display Indicato BTL Bottle ADLS Aircraft Data Log Sheet BTMS Brakes Temperature Monitoring System ADS-B Automatic Dependent Surveillance - Broadcast BRNAV Basic Area Navigation ADS-C Automatic Dependent Surveillance - Contract CAS Crew Alerting System AED Automatic External Defibrillator CB(s) Circuit Breaker(s) AFIS Airborne Flight Information System CCD Cursor Control Device AFM Aeroplane Flight Manual CDL Configuration Deviation List AGL Above Ground Level CDTI Cockpit Display and Traffic Information AIL Aileron CDU Control Display Unit ALRT Alert CH Channel ALT Alternate/Altitude CHGR Charger AMP Ampere CHRG Charge AMM Aircraft Maintenance Manual CHRGR Charger ANNUN Annunciator CKPT Cockpit AOA Angle of Attack CLSD Closed AOM Aeroplane Operating Manual CMD Command AP Autopilot CMF Communications Management Function APP Approach CMU Communications Management Unit APU Auxiliary Power Unit COMM Communication(s) ASC Aircraft Service Change CONT Control ASCB Avionics Standard Communication Bus CPAM Cabin Pressure Acquisition Module ATC Air Traffic Control CPCS Cabin Pressure Controller System AUTO Automatic CPDLC Controller-Pilot Data Link Communications

22 ACRONYMS AND ABBREVIATIONS CPOP Copilot's Overhead Circuit Breaker Panel EPMP Electrical Power Monitor Panel CTL Control EPR Engine Pressure Ratio CTLR Controller ER Extended Range CVFDR Cockpit Voice Flight Data Recorder Combo ESS Essential CVR Cockpit Voice Recorder EVAS Emergency Vision Assurance System DA Decision Altitude EVS Enhanced Vision System DAU(s) Data Acquisition Unit(s) EXT Extinguisher DBDI Digital Bearing Distance Indicators FAA Federal Aviation Administration DC(s) Display Controller(s) FAK First Aid Kit DC Direct Current FALT Fault DDA Digital Discrete Adapter FDR Flight Director Recorder DDRMI Dual Digital Radio Magnetic Indicator FGC Flight Guidance computer DISENG Disengaged FGS Flight Guidance System DISP Display FL Flight Level DL Data Loader FLCH Flight Level Change DME Distance Measuring Equipment FLTA Forward Looking Terrain Avoidance DU(s) Display Unit(s) FMS Flight Management System ECM Electronic Control Mode FPA Flight Path Angle ECS Environmental Control System FREQ Frequency ECU Electronic Control Unit FSS Flight Service Station EFB Electronic Flight Bag FWC Fault Warning Computer(s) EFIS Electronic Flight Information System FWD Forward EFVS Enhanced Flight Vision System GIV Gulfstream IV Aircraft EGPWS Enhanced Ground Proximity Warning Systems GNSSU Global Navigation Satellite Sensor Unit EGT Exhaust Gas Temperature GPS Global Positioning System EICAS Engine Instruments and Crew Alerting System GPWS Ground Proximity Warning System E INV Emergency Inverter HDG Heading ELT Emergency Locator Transmitter HF High Frequency ELWS Electrical Load Warning System HP High Pressure EMK Emergency Medical Kit HUD Head-up Display EMS Emergency Medical System HYD Hydraulic EPA Environmental Protection Agency HZ Hertz (circles per second)

23 ACRONYMS AND ABBREVIATIONS ICAO International Civil Aviation Organization MSL Mean Sea Level IFR Instrument Flight rules MSU Mode Select Unit IGN Ignition NAT MNPS North Atlantic Minimum Performance Navigation Specification ILS Instrument Landing System NAV Navigation INBD Inboard NAVAID Navigation Aid INHIB Inhibit ND Navigation Display INOP Inoperative NEF Non-Essential Equipment and Furnishings IRCM InfraRed Counter Measure System NICAD Nickel Cadmium IRS(s) Inertial Reference System(s) NLG Nose Landing Gear IRU Inertial Reference Unit NM Nautical Mile(s) ISDU Inertial Sensor Display Unit NOTAMS Notice To Airmen KHZ kilohertz NVG Night Vision Goggles LDG Landing NWS Nose Wheel Steering LED(s) Light-Emitting Diode(s) OAT Outside Air Temperature LNAV Lateral Navigation ORIDE Override LPV Localizer Performance with Vertical guidance OTBD Outboard LRCS Long Range Communications System OVERTEMP Overtemperature LSS Lightning Sensor System OVHD Overhead LVT Linear Variable Transducer OVHT Overheat MAX Maximum OVRD Override MDA Minimum Descent Altitude OXY Oxygen MEL Minimum Equipment List PA Passenger Address MIC(s) Microphone(s) PAX Passenger MISCMP Miscomparison PCMCIA Personal Computer Memory Card International Association MISCOMP Miscomparison PDA Premature Descent Alert MLS Microwave Landing System PDB Power Distribution Box MMEL Master Minimum Equipment List PDE Protective Breathing Equipment MNPS Minimum Navigation Performance Specifications PERF Performance MSA Minimum Safe Altitude PF Pilot Flying PFD(s) Primary Flight Display(s) STBY Standby PIC Pilot In Command STC Supplemental Type Certificate PM Pilot Monitoring SWLP Standby Warning Lights Panel

24 ACRONYMS AND ABBREVIATIONS PNF Pilot Not Flying SYM Symbol POP Pilot s Overhead Circuit Breaker Panel SYS System PRNAV Precision-Area Navigation T/O Takeoff PSU Personal Service Unit T/O APP Takeoff/Approach PTT Push-To-Talk T/R Thrust Reverser PWR Power T/REV Thrust Reverser QRH Quick Reference Handbook TA Traffic Alert R Right TACAN Tactical Air Navigation RA Resolution Advisory TAS True Airspeed RAD ALT Radio Altimeter TAT Total Air Temperature RAAS Runway Awareness & Advisory System TAWS Terrain Awareness and Warning System REF Reference TCAS Traffic Alert and Collision Avoidance RMI Radio Magnetic Indicator TCS Touch Control Steering RNAV Area Navigation TEMP(s) Temperature(s) RNP Required Navigation Performance TGT Turbine Gas Temperature RPM Revolutions Per Minute THROT Throttle RT Receiver-Transmitter TO/GA Takeoff/Go-Around RTU Radio Tuning Unit TOGA Takeoff/Go-Around RVSM Reduced Vertical Separation Minimum TOGW Takeoff Gross Weight SATCOM Satellite Communication TR(s) Thrust Reverser(s) SATVOICE Satellite Voice TRU Transformer-Rectifier Unit SBAS Satellite-Based Augmentation System UHF Ultra High Frequency SEL Select V1 Takeoff Decision Speed (Knots) SELCAL Selective Calling V2 Takeoff Safety Speed (Knots) SG(s) Symbol Generator(s) VA Maneuvering Speed (Knots) SN Serial Number VFE Maximum Flaps Extended Speed (Knots) SOV(s) Shutoff Valve(s) VFR Visual Flight Rules SPDBRK Speed Brake VFS Flight Safety Speed (Knots)

25 ACRONYMS AND ABBREVIATIONS VHF VLE VLO VLV VMC VMO VNAV VOL VOR VR VREF VS WAAS WHL WOW WSHLD WX XM YD Very High Frequency Maximum Landing Gear Extended (Knots) Maximum Landing Gear Operation Speed (Knots) Valve Minimum Control Speed (Knots) Maximum Operating Limit Speed (Knots) Vertical Navigation Volume Very High Frequency, Omni-Range Rotation Speed (Knots) Reference Speed (Knots) Stall Speed (Knots) Wide Area Augmentation System Wheel Weight On Wheels Windshield Weather Extended Module Yaw Damper

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27 SECTION ONE LINE REPLACEABLE UNIT (LRU) COMPONENT RELIEF

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29 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AIR CONDITIONING 1. Cabin Altitude Indication (Overhead Panel) (continued) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 1 0 May be inoperative provided cabin altitude is available on EICAS Synoptic display. C 1 0 May be inoperative provided: a) Cabin Pressure Selector Panel is operative, and b) Pressurisation is operated in AUTO mode. C 1 0 (O) May be inoperative provided: a) Cabin Differential Pressure Indicator is operative, and b) A chart is provided to crew to convert Cabin Differential Pressure to Cabin Altitude. D 1 0 May be inoperative provided aeroplane is equipped with additional pneumatic threein-one cabin pressurisation monitoring instrument, and Cabin Altitude Indicator portion is fully operative. be placed adjacent to Cabin Altitude Indicator and will be noted on be placed adjacent to Cabin Altitude Indicator and will be noted on Flight crew shall refer to the AOM Section , Figure 10. be placed adjacent to Cabin Altitude Indicator and will be noted on be placed adjacent to Cabin Altitude Indicator and will be noted on

30 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AIR CONDITIONING 1. Cabin Altitude Indication (Overhead Panel) (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 1 0 (O) May be inoperative provided aeroplane is operated in unpressurised configuration. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed adjacent to Cabin Altitude Indicator and will be noted on

31 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AIR CONDITIONING 2. Cabin Differential Pressure Indication (Overhead Panel) (continued) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D 1 0 May be inoperative provided cabin differential pressure is available on EICAS Synoptic display. C 1 0 May be inoperative provided: a) Cabin Pressure Selector Panel is operative, and b) Pressurisation is operated in AUTO mode. D 1 0 (O) May be inoperative provided: a) Cabin Altitude Indicator is operative, and b) A chart is provided to crew to convert Cabin Altitude to Cabin Differential Pressure. D 1 0 May be inoperative provided aeroplane is equipped with additional pneumatic threein-one cabin pressurisation monitoring instrument, and Cabin Altitude Indicator portion is fully operative. be placed adjacent to Cabin Differential Pressure Indicator and will be noted on be placed adjacent to Cabin Differential Pressure Indicator and will be noted on Flight crew shall refer to the AOM Section , Figure 10. be placed adjacent to Cabin Differential Pressure Indicator and will be noted on be placed adjacent to Cabin Differential Pressure Indicator and will be noted on

32 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AIR CONDITIONING 2. Cabin Differential Pressure Indication (Overhead Panel) (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 1 0 (O) May be inoperative provided aeroplane is operated in unpressurised configuration. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed adjacent to Cabin Differential Pressure Indicator and will be noted on 3. Cabin Rate of Climb Indicator D 1 0 be placed adjacent to Cabin Rate of Climb Indicator and will be noted on

33 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING 4. Automatic Pressurisation Control Systems MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 B 2 0 (O) Except for ER operations, may be inoperative provided: a) Manual Pressurisation Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, and e) Aeroplane is operated in accordance with AFM Limitations. Flight crew will ensure required items e.g. Manual Pressurisation Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. AFM, Section 2, Normal Procedures, Before Starting Engines. Flight crew will operate aeroplane in accordance with AFM, Section 1, Limitations, Cabin Pressurisation Control and Section 3, Abnormal Procedures, Loss of Automatic Pressurisation Control. For Taxi, Takeoffs and Landings - Max Cabin Pressure Differential 0.3 psi. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. An Inoperative Placard stating AUTO INOP will be placed above FAULT / MANUAL Switch and will be noted on (continued) Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft.

34 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING 4. Automatic Pressurisation Control Systems (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 B 2 0 (O) Except for ER operations, may be inoperative provided aeroplane is operated in unpressurised configuration. None required To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. An Inoperative Placard stating "AUTO INOP" will be placed above FAULT/ MANUAL Switch and will be noted on 5. Manual Pressurisation Control System 6. Semi-Auto Pressurisation Control System C 1 0 May be inoperative provided both Automatic Pressurisation Control Systems are operative. be placed in a prominent C 1 0 be placed in a prominent

35 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING 7. Cabin Altitude Pressure Warning System MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 May be inoperative provided: a) Cabin Altitude and Differential Pressure Indicators are operative, b) Cabin Oxygen On Warning System is operative, and c) Aeroplane is operated in accordance with AFM Limitations. C 1 0 (O) May be inoperative provided aeroplane is operated in unpressurised configuration. be placed in a prominent position to be seen by the flight crew and will be noted on To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed in a prominent position to be seen by the flight crew and will be noted on 8. Pressurisation Outflow Valve Position Indicator C 1 0 May be inoperative provided all other components of the Cabin Pressure Control Panel and Cabin Pressure Indicator are operative. be placed on Outflow Valve Position Indicator and will be noted on

36 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-8 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING 9. Cockpit Zone Temperature Control System & Cabin Zone Temperature Control Systems MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 3 2 C 3 1 (O) May be inoperative provided: a) Ram Air system is operative, and b) Aeroplane is operated in unpressurised configuration. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed adjacent to Cockpit/Cabin Temperature Indicator and will be noted on 1) Automatic System C 3 0 May be inoperative provided: a) Associated manual control system is operative, and b) Associated temperature indicator is operative. 2) Manual Systems C 3 0 May be inoperative provided: a) Associated automatic control system is operative, and b) Associated temperature indicator is operative. be placed on AUTO half of capsule of Cockpit/Cabin Temperature Selectors and will be noted on be placed on MANUAL half of capsule of Cockpit/Cabin Temperature Selectors and will be noted on

37 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 21-9 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING 10. Cockpit/Cabin Zone Temperature Indicators (Overhead Panel) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D 3 0 May be inoperative provided associated Automatic Temperature Control System is operative. be placed on affected Temperature Indicator face and will be noted on D 3 0 May be inoperative provided associated zone temperature is available on EICAS Synoptic display. D 3 0 May be inoperative provided associated Manual Temperature Control System is operative. be placed on affected Temperature Indicator face and will be noted on be placed on affected Temperature Indicator face and will be noted on 11. Duct Temperature Indicators (Overhead Panel) D 3 0 be placed on overhead panel below the Zone/Duct Switch and will be noted on

38 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AIR CONDITIONING 12. Environmental Control System (ECS) Packs 1) Pressurized Configuration 2) Unpressurised Configuration MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 2 1 Except for ER operations, may be inoperative provided: a) Inoperative ECS Pack is selected OFF, b) Bleed Air Isolation Valve is CLOSED and OPERATIVE, c) Right Main TRU is operative, d) Aeroplane is operated at or below FL410, e) Autothrottle must be operative and engaged at or above FL400, a nd f) Aeroplane is operated in accordance with AFM Limitations. C 2 0 (O) Except for ER operations, may be inoperative provided Outflow Valve is operative. be placed adjacent to affected "ECS PACK" Switch and will be noted on To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed adjacent to affected "ECS PACK" Switches and will be noted on

39 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AIR CONDITIONING 13. Three-In-One Cabin *** Pneumatic Pressurisation Monitoring Instrument (located in instrument panel or pedestal) 14. Air Conditioning System Pack Inlet Valves MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 1 0 May be inoperative provided primary Cabin Altitude and primary Cabin Differential Pressure Indicators are operative either in the overhead panel or on the Synoptic Display. C 2 1 (M) Except for ER operations, may be inoperative provided: a) Affected Valve is CLOSED and deactivated electrically, b) Associated Air Conditioning Pack is selected OFF, and c) Aeroplane is operated in accordance with AFM Limitations. be placed on Three-In-One Cabin Pneumatic Pressurisation Monitoring Instrument face and will be noted on Maintenance will ensure affected Valve is "CLOSED" and electrically deactivated when associated Air Conditioning Pack switch is selected "OFF". Associated Air Conditioning CB must NOT be pulled. AMM, chapter Flight crew may perform maintenance function if maintenance is unavailable. Flight crew may accomplish this task if properly qualified and authorised. CAUTION: Pulling (de-energizing) associated Air Conditioning CB will cause valve to open, allowing airflow to restart. be placed on or below affected ECS Pack Switch and will be noted on

40 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AIR CONDITIONING MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 15. Outflow Valve System C 1 0 (M) (O) May be inoperative provided: a) Outflow valve is positioned to full OPEN position and electrically isolated, b) Aeroplane is operated in unpressurised configuration, and c) Overwater flights beyond 30 minutes at normal cruising speed or 50 NM away from land, whichever is the lesser are prohibited. Maintenance will ensure Outflow Valve is positioned to full OPEN position and electrically de-energized by pulling the Cab Press Man Cont breaker LEER E-8. Flight crew may accomplish this task if properly qualified and authorised. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed in a prominent 1) AC Motors C 2 1 May be inoperative provided: a) DC motor is operative, and b) Aeroplane is operated in accordance with AFM Limitations. be placed in a prominent

41 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING 16. Pressure Relief Valve MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 (O) May be inoperative provided: a) Cabin differential pressure and cabin altitude displays are operative, b) Selected cabin altitude is 1,000 feet higher than normal cabin altitude for the cruise flight level, and c) Flight crew monitors actual cabin differential pressure and maintains it at or below 9.5 psi. C 1 0 (O) May be inoperative provided aeroplane is operated in unpressurised configuration. Flight Crew will ensure: a) Cabin Differential Pressure and Cabin Altitude Displays are operative. b) Select Semi-Auto Operation and selected Cabin Altitude is 1,000 feet higher than normal Cabin Altitude for cruise flight level. c) Monitor actual Cabin Differential Pressure and maintain it at or below 9.5 psi. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed on Cabin Pressure Control Panel and will be noted on be placed on Cabin Pressure Control Panel and will be noted on

42 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING 17. Cabin Pressure Indicator and Control Panel MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 Any one switch or indicator may be inoperative for dispatch. 1) Manual Light C 1 0 be placed on Control Panel and will be noted on 2) Flight/Landing Switch (Light Function Only) C 1 0 be placed on Control Panel and will be noted on 3) Fault/Manual Switch (Light Function Only) 4) Auto/Semi Switch (Light Function Only) 18. Selector Panel (Semi-Auto) 19. Remote Filter (Pressure Relief Valve PRV) C 1 0 be placed on Control Panel and will be noted on C 1 0 be placed on Control Panel and will be noted on B 1 0 May be inoperative provided: a) Auto system (Cabin Pressure Control Panel) is operative, and, b) Semi-auto mode is considered inoperative. be placed on Selector Panel and will be noted on B 1 0 A Placard indicating filter is removed will be displayed in a prominent position to be seen by flight crew and will be noted on

43 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING 20. CPAM (Cabin Pressure Acquisition Module) 21. Ram Air System 1) Pressurized Configuration 2) Unpressurised Configuration MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 May be inoperative provided both auto systems are operative. C 1 0 May be inoperative provided: a) Automatic Pressurisation Control System is operative, b) Manual Pressurisation Control System is operative, c) Bleed Air Pressure Regulating and Shut-Off Systems are operative, and d) Aeroplane is operated in accordance with AFM Limitations and Procedures. C 1 0 (O) May be inoperative provided: a) Aircraft is operated in unpressurised configuration, and b) Aeroplane is operated in accordance with AFM Limitations and Procedures. be placed adjacent to the Ram Air Switch to be viewed by the flight crew and will be noted on the ADLS To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed adjacent to the Ram Air Switch to be viewed by the flight crew and will be noted on the

44 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 21. AIR CONDITIONING MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ PSU Fan C 1 0 (O) May be inoperative provided: a) Ambient Temperature is 95 degrees F (35 degrees C) or cooler, b) TRU electrical loads are 50% or less, c) Right main TRU is operative, and d) Both Environmental Control System (ECS) Packs are operative. Flight crew will: a) Minimize ground operation time, especially during hot weather. b) During Ground operation, monitor TRU load limit load to 50%. c) For ground operation longer than 15 minutes ensure main and baggage doors are closed, APU air is selected ON and outflow valve is fully OPEN.

45 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 22-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 22. AUTO FLIGHT MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ Autothrottle Systems C Performance Management Systems (SmartPerf/TOLD) (GV) C 2 0 May be inoperative provided Quick Reference Handbook is immediately available to the flight crew. (GV-SP / GIV-X) C 2 0 May be inoperative provided Performance Handbook is immediately available to the flight crew. 3. Control Wheel Autopilot Disconnect Buttons C 2 1 May be inoperative provided: a) Autopilot is not used below 1,500 feet AGL, b) Approach minimums do not require the use of the autopilot, and c) Aeroplane is piloted from the side with operative button.

46 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 22-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AUTO FLIGHT 4. Autothrottle Disconnect Buttons (On Thrust Lever Handles) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 2 1 (O) One may be inoperative provided functionality of remaining Autothrottle Disconnect Button is checked prior to each departure. With both engines running, taxi aeroplane to an area where engine run-ups are allowed on airport. Prior to performing the test, access TRS menu on the Display Controller. Select Manual EPR and set a target of Once in position, increase thrust on both engines to 1.10 EPR. Engage autothrottle in the standard manner. Once engaged, use the operative disconnect switch to disengage autothrottle. Verify that the autothrottle is disengaged by listening for disconnect tone and retard both throttles to idle. Again, increase thrust on both engines to 1.10 EPR. Engage autothrottle in the standard manner. Once engaged, manually override autothrottle by pulling forcefully (approximately 25 lb of force is required) aft on throttles. Verify that autothrottle is disengaged by listening for disconnect tone and retard both throttles to idle.

47 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 22-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AUTO FLIGHT 5. Autothrottle Engage / Disengage Switches (On Thrust Lever Stem) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 2 1 (O) One may be inoperative provided functionality of remaining Autothrottle Engage/Disengage Switch is checked prior to each departure. With both engines running, taxi the aeroplane to an area where engine run-ups are allowed on airport. Prior to performing the test, access the TRS menu on the Display Controller. Select Manual EPR and set a target of Once in position, increase thrust on both engines to 1.10 EPR. Engage autothrottle in the standard manner. Once engaged, use the operative engage/disengage switch to disengage autothrottle. Verify that autothrottle is disengaged by listening for disconnect tone and retard both throttles to idle. Again, increase thrust on both engines to 1.10 EPR. Engage autothrottle in the standard manner. Once engaged, manually override autothrottle by pulling forcefully (approximately 25 lb of force is required) aft on throttles. Verify that autothrottle is disengaged by listening for disconnect tone and retard both throttles to idle. be placed on Thrust Lever Stem and will be noted on

48 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 22-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AUTO FLIGHT 6. Touch Control Steering Switches (TCS) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D Autopilots (Flight Guidance Computers (FGC) / Flight Directors) C 2 1 (M) (O) Except for ER operations or where en route operations or approach minimums require its use, may be inoperative provided aeroplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative. Maintenance will pull and reset the affected IAC (GV) or MAU Channel (GV-SP/GIV-X) and Guidance Panel circuit breakers in attempt to reset the AP/FGC. If AP/FGC does not recover, no further action required. Flight crew will observe AFM limitations in the event the operative FGC fails and the Yaw Damper is inoperative. NOTE: AP/FGC is required for MNPS, RVSM, RNP and PRNAV operations. 8. Yaw Damper Systems C 2 1 (O) Except for ER operations, may be inoperative provided aeroplane is operated in accordance with AFM Limitations. Flight crew will ensure aeroplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. AN Inoperative Placard will position to be viewed by the flight crew and will be noted on the

49 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 22-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AUTO FLIGHT 9. Takeoff/Go-Around (TO/GA) Buttons (on Power Lever Handles) (continued) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 2 1 (O) May be inoperative provided approach minimums do not require its use. Flight Director is not available for Takeoff or Go-Around with both TOGA buttons inoperative. Flight crew shall use raw data and manual throttles for takeoff and go-around. For takeoff, once airborne and above 500 ft AGL, pilot monitoring (PM) shall select desired lateral mode (HDG or LNAV) on guidance panel as directed by pilot-flying (PF). Additionally, PNF shall select desired vertical mode (FLCH or VS or FPA) and engage auto-throttle as directed by PF. For go-around, after flaps and landing gear have been retracted and aeroplane is above 500 ft AGL, PNF shall select desired lateral mode (HDG or LNAV) and vertical mode (FLCH or VS or FPA) on guidance panel and engage auto-throttle at direction of PF. position to be viewed by the flight crew and will be noted on

50 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 22-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: AUTO FLIGHT 9. Takeoff/Go-Around (TO/GA) Buttons (on Power Lever Handles) (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 2 0 (O) May be inoperative provided: a) Both power levers are operated manually for takeoff and go-around, and b) Autopilot and Flight Director are not used below 500 feet or MDA, whichever is higher. NOTE 1: Flight Director Takeoff and Go- Around guidance and Autothrottles are not available with both TO/GA switches inoperative. NOTE 2: TO/GA system is required for RNP AR operations. Flight Director and Autothrottle are not available for Takeoff or Go-Around with both TO/GA buttons inoperative. Flight crew shall use raw data and manual throttles for takeoff and goaround. For takeoff, once airborne and above 500 ft AGL, pilot-not-flying (PNF) shall select desired lateral mode (HDG or LNAV) on guidance panel as directed by pilot-flying (PF). Additionally, PNF shall select desired vertical mode (FLCH or VS or FPA) and engage autothrottle as directed by PF. For go-around, after flaps and landing gear have been retracted and aeroplane is above 500 ft AGL, PNF shall select desired lateral mode (HDG or LNAV) and vertical mode (FLCH or VS or FPA) on guidance panel and engage autothrottle at direction of PF. position to be viewed by the flight crew and will be noted on

51 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 22-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 22. AUTO FLIGHT 10. Mach Trim Systems (GV-SP/GIV-X only) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 2 1 position to be viewed by the flight crew and will be noted on

52 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 23. COMMUNICATIONS 1. Radio Communications (VHF, UHF) 1) VHF Communications *** a) Frequency Transer Light *** b) Frequency Transfer Switch *** c) Frequency Selector Knob *** d) Frequency Indication MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C - 1 Any in excess of one, and not powered by an emergency bus, may be inoperative provided flight is conducted under VFR over routes navigated by reference to visual landmarks. C - 2 Any in excess of two, and not powered by an emergency bus, may be inoperative. NOTE: Comm 1 is powered by the Emergency Bus. be placed adjacent to affected Radio Frequency Management Unit (GV) or MCDU (GVSP/GIV-X) and will be noted on be placed adjacent to affected Radio Frequency Management Unit (GV) or MCDU (GVSP/GIV-X) and will be noted on C - 0 One or more may be inoperative. C - 0 One or more may be inoperative. C - 2 Any in excess of two may be inoperative. C - 2 Any in excess of two may be inoperative.

53 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: COMMUNICATIONS MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 2. Cockpit Voice A A - 0 One or more may be inoperative provided: Recorder System a) Not more than 72 hours have elapsed since cockpit voice recorder was found to be unserviceable, b) Aeroplane does not exceed 8 further consecutive flights with cockpit voice recorder unserviceable, and c) Any flight data recorder required to be carried is operative. 1) Independent Power *** Source C 1 0

54 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 23. COMMUNICATIONS 3. Selective Call *** System (SELCAL) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C - 0 (O) May be inoperative provided alternate procedures are established and used. One crew member shall monitor the appropriate frequency. D - 0 May be inoperative provided procedures do not require its use. 1) Channels C - 0 (O) May be inoperative provided alternate procedures are established and used. Flight crew will ensure: a) SELCAL decoder monitors audio from the VHF and HF communications transceivers, b) Recognizes receipt of the tone set assigned to the aeroplane, and c) Provides the flight compartment with call alert signals. D - 0 May be inoperative provided procedures do not require its use.

55 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 23. COMMUNICATIONS 4. Emergency Locator Transmitters (ELT) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 *** 1) Survival Type ELTs D - - (M) Any in excess of those required may be missing or inoperative provided inoperative equipment is placarded inoperative, removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit. Maintenance will ensure to placard inoperative survival type ELT and remove from aeroplane for servicing. Flight crew may accomplish this task if properly qualified and authorised. *** 2) Fixed ELTs A - 0 May be inoperative for a maximum of 6 flights or 25 flying hours, whichever occurs first. D - - Any in excess of those required may be missing.

56 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 23. COMMUNICATIONS 5. Crewmember *** Interphone System 1) Passenger Configuration a) Flight Deck to Cabin, Cabin to Flight Deck Functions b) Cabin to Cabin Functions c) Flight Deck to Ground MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 B - - (O) May be inoperative provided: a) Alternate procedures are established and used for communications with flight deck, and b) PA system is operative. NOTE: Any station function(s) that is operative may be used. C - 0 (O) May be inoperative provided: a) Alternate, normal and emergency procedures are established and used, and b) PA system is operative. NOTE: Any station function(s) that is operative may be used. C - 0 May be inoperative provided alternate, normal and emergency procedures are established and used. D - 0 May be inoperative provided procedures do not require its use. Flight crew may use the PA to communicate with the cabin crew or speak to the cabin crew directly in either the cockpit or cabin to pass information. Cabin crew may use the PA to communicate with the cabin crew or speak to the cabin crew directly in either the cockpit or cabin to pass information. be placed on Interphone System and will be noted on be placed on Interphone System and will be noted on be placed on Interphone System and will be noted on be placed on Interphone System and will be noted on

57 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 23. COMMUNICATIONS 6. Interphone Systems *** MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D - 0 be placed on Flitephone System and will be noted on 7. Cockpit Speakers C 2 0 May be inoperative provided: a) Affected speaker is not required for aural warnings, and b) An operative headset is provided for each person on cockpit duty.

58 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: COMMUNICATIONS 8. Passenger Address *** Systems (PA) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: Passenger Configuration B 1 0 (O) May be inoperative provided: a) Alternate, normal, and emergency procedures, and/or operating restrictions are established and used, and b) Flight attendant alerting system (audio and visual) operates normally. NOTE: Any station function(s) that is operative may be used. C 1 0 (O) May be inoperative provided: a) PA not required by Operating Requirements, and b) Alternate, normal and emergency procedures, and/or operating restrictions are established and used. NOTE: Any station function(s) that is operative may be used. Lavatory Speakers C - - (O) May be inoperative provided alternate procedures are established and used. Cargo Only Configuration D 1 0 May be inoperative provided procedures do not require its use. Flight crew will coordinate with cabin crew prior to the flight. Flight crews may use the flight deck-to-cabin interphone system to pass information to the cabin crew. Also, the flight crew may speak to the cabin crew directly in either the cockpit or cabin to pass information. Flight crew will coordinate with cabin crew prior to the flight. Flight crews may use the flight deck-to-cabin interphone system to pass information to the cabin crew. Also, the flight crew may speak to the cabin crew directly in either the cockpit or cabin to pass information. Flight crew will ensure alternate procedures are established and used.

59 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-8 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 23. COMMUNICATIONS 9. Satellite *** Communication Systems 10. Prerecorded *** Passenger Announcement Systems 11. Hand Held Microphones MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D - 0 May be inoperative provided procedures do not require their use. D - 0 (O) May be inoperative provided alternate procedures are established and used. D - 0 May be inoperative provided: a) Each cockpit crewmember uses a boom microphone, and b) Each (Control Wheel) Press-to-Talk Switch is operative. 12. Headsets D - - Any in excess of one headset (including boom microphone) for each required crewmember on flight deck duty may be inoperative or missing. 13. Right Side Radio Frequency Management Unit (RFMU) (GV) C 1 0 May be inoperative provided: a) Cross-side tuning function of the left RFMU is operative, b) Radio tuning function of both FMS s are operative, and c) Inoperative RFMU is selected OFF. Flight crew will comply with proviso in remarks column by using manual PA system to inform passengers. In addition, the flight crew or cabin crew may give direct oral instructions to the passengers.

60 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 23-9 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 23. COMMUNICATIONS 14. Alerting Systems *** (Audio/Visual) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C - - Visual signal may be inoperative on flight deck. C - - Both visual and aural signals may be inoperative in cabin provided PA system is operative from flight deck. NOTE: Any station function(s) that is operative may be used. 15. Handset Systems C - - Handset at non required stations may be inoperative. C - - (O) One handset may be inoperative provided alternate procedures are established and used to compensate for the loss of PA and interphone function at the affected station. NOTE: Any handset in excess of that required at each station may be inoperative. Flight crew will use the PA or direct oral communications as necessary.

61 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: COMMUNICATIONS 16. High Frequency (HF) Communication Systems MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D - - Any in excess of those required by Operating Requirements may be inoperative. C 2 1 (O) May be inoperative while conducting operations that require two LRCS provided: a) Aircraft SATVOICE system operates normally, b) Alternate procedures are established and used, c) SATVOICE services are available as a LRCS over the intended route of flight, and d) The ICAO Flight Plan is updated (as required) to notify ATC of the communications equipment status of the aircraft. be placed adjacent to affected Interphone System and will be noted on The flight crew shall perform the SATVOICE preflight test on the Datalink Manager menu. Refer to the OM for additional details. For GV, the crew will perform a Satvoice datalink and voice call prior to departure.

62 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: COMMUNICATIONS 17. NAVCOM Radio (GV-SP, GIV-X) 18. Audio Interface Units (AIUs) (GV only) 19. Datalink System *** (GV) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 1 0 May be inoperative provided operations do not require its use. B 2 1 May be inoperative provided flight does not require use of HF radio. C - 0 (O) May be inoperative provided alternate procedures are established and used. NOTE 1: Datalink system is required for ADS-C and/or CPDLC operations. NOTE 2: Datalink must be operative whenever flights in RNP 4 airspace are conducted. D - 0 May be inoperative provided routine procedures do not require its use. NOTE 1: Datalink system is required for ADS-C and/or CPDLC operations. NOTE 2: Datalink must be operative whenever flights in RNP 4 airspace are conducted. Flight crew will voice over VHF/HF to relay pertinent information to the air traffic management system.

63 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: COMMUNICATIONS 20. Modular Radio Cabinet (MRC) Power Supplies (GV-SP, GIV-X) 21. Communications *** Management Function / CMF (GV-SP/GIV-X) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: A 2 1 May be inoperative provided: a) Associated Comm and Nav radios and opposite ATC are operative, and b) Repairs are made within one flight day. NOTE: Dispatch is acceptable witha MRC 1 or MRC 2 failed and EICAS blue message APM FAIL and ASCB FAIL displayed. C - 0 (O) May be inoperative provided alternate procedures are established and used. NOTE 1: Datalink system is required for ADS-C and / or CPDLC operations. NOTE 2: Datalink must be operative whenever flights in RNP 4 airspace are conducted. D - 0 May be inoperative provided routine procedures do not require its use. NOTE 1: Datalink system is required for ADS-C and / or CPDLC operations. NOTE 2: Datalink must be operative whenever flights in RNP 4 airspace are conducted. Flight crew will use voice over VHF/HF to relay pertinent information to the air traffic management system.

64 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: COMMUNICATIONS 22. Controller Pilot Data *** Link Communications (CPDLC) 1) ATN B1 *** (PM-CPDLC / Link 2000+) 2) FANS 1/A *** (ADS-C/CPDLC) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D 1 0 (O) May be inoperative provided en route operations do not require its used. D 1 0 (O) May be inoperative provided en route operations do not require its used. Flight crew will use voice over VHF/HF or SATVOICE to relay pertinent information to the air traffic management system. Flight crew will use voice over VHF/HF or SATVOICE to relay pertinent information to the air traffic management system.

65 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ELECTRICAL POWER MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 1. Engine Generators B 2 1 Except for ER operaations, may be inoperative provided: a) APU Generator is used for all phases of flight, b) Aeroplane is operated at or below FL450, and c) Standby Electrical System is operative. (GIV-X) B 2 1 (O) Except for ER operations, may be inoperative provided: a) APU Generator is used for all phases of flight, b) Aeroplane is operated at or below FL 450, c) Standby Electrical System is operative, and d) FSECU SPOST is performed manually prior to the first flight of the day for aeroplanes equipped with ASC 086 and dispatching with the left generator inoperative. be placed above affected Generator Switch on Electric Power Control Panel (EPCP) and will be noted on a) AUX PUMP.ON b) STAB PRI AC CB (POP D-2)...CLOSED c) STAB SEC AC CB (CPOP D-2)..CLOSED d) FLAP / STAB PRI L DC CB (POP C-6).. PULL e) FLAP / STAB SEC DC CB (POP E-1).PULL f) FLAP / STAB PRI R DC CB (CPOP C-6).PULL g) FLAP / STAB PRI R DC CB (CPOP C-6), FLAP / STAB SEC DC CB (POP E-1) RESET...(SIMULTANEOUSLY) h) FLAP / STAB PRI L DC CB (POP C-6).RESET IF FLAPS FAILED (AMBER) AND STABILIZER FAILED (AMBER) CAS MESSAGES DO NOT CLEAR WITHIN 90 SECONDS, MAINTENANCE IS REQUIRED PRIOR TO DISPATCH. i) AUX PUMP...OFF be placed above affected Generator Switch on Electric Power Control Panel (EPCP) and will be noted on

66 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ELECTRICAL POWER MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 2. APU Generator B 1 0 (M) Except for ER operations, may be inoperative provided APU is not used. 3. Transformer-Rectifier Units (TRUs) 4. Main Aeroplane Battery Chargers B 5 4 (M) May be inoperative provided: a) Both Generators are operative, b) Both essential TRUs are operative, c) Auxiliary TRU is operative, d) APU Generator is operative, e) Both Battery chargers are operative, f) Both Main Aeroplane Batteries are operative, and g) Inoperative TRU circuit breaker on the Power Distribution Box is pulled and collared. B 2 1 (M) May be inoperative provided: a) Both Engine Generators are operative, b) APU Generator is operative, c) Associated Battery Charger circuit breaker on the Power Distribution Box is pulled and collared, and d) Standby Electrical System is operative. Maintenance will pull and collar APU CONT #1 left EER C-13 and APU CONT #2 right EER C-11. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will pull and collar affected TRU CONTROL CB on Power Distribution Box (PDB). Maintenance will ensure AUX TRU is operative and both essential TRUs are operative. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will pull and collar CB of associated Battery Charger (located on PDB). Maintenance can verify associated Battery Charger by utilizing Operational Test located in AMM Chapter Flight crew may accomplish this task if properly qualified and authorised. be placed above AUX PWR Switch on EPCP and will be noted on be placed in a prominent be placed above Battery Charger Circuit Breakers and will be noted on

67 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 24. ELECTRICAL POWER 5. Main Aeroplane Batteries MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 B 2 1 (M) May be inoperative provided: a) There are no other electrical power source failures, b) Associated Battery cables are disconnected and secured, c) Associated Battery Charger circuit breaker on the Power Distribution Box is pulled and collared, and d) Associated battery circuit breaker is pulled and collared. B 2 1 (M)(O) May be inoperative provided: a) Aeroplane is operated in day VMC, b) Standby Electrical System is operative, c) Associated Battery cables are disconnected and secured, d) Associated Battery Charger circuit breaker on the Power Distribution Box is pulled and collared, and e) Associated battery circuit breaker is pulled and collared. Maintenance will ensure: a) Standby Electrical System is operative, b) Pull and collar associated "BATT CHGR" and "BATT CONT" CB, and c) Associated battery cables will be disconnected and secured. Refer to AMM chapter Maintenance will pull and collar associated "BATT CHGR" and "BATT CONT" CB. In addition, associated battery cables will be disconnected and secured. Refer to AMM chapter Flight crew will ensure aeroplane is operated in day VMC only. be placed on affected "BATT 1, BATT 2" Master Switch on the Electric Master Panel and will be noted on be placed on affected "BATT 1, BATT 2" Master Switch on the Electric Master Panel and will be noted on

68 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ELECTRICAL POWER 6. Battery Ammeters (Overhead Panel) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 2 0 May be inoperative provided: a) Associated voltmeter is operative, and b) Both battery charger fail messages are operative. C 2 0 May be inoperative provided battery ammeter indications are available in EICAS. (EICAS Indication) C 2 0 May be inoperative provided battery ammeter in overhead panel are operative. 7. Battery Voltmeters (Overhead Panel) C 2 0 May be inoperative provided associated ammeter is operative. C 2 0 May be inoperative provided Battery Voltmeter indications are available on EICAS. (EICAS Indication) C 2 0 May be inoperative provided Battery Ammeter indications are available on EICAS. C 2 0 May be inoperative provided Battery Voltmeters in overhead panel are operative. be placed on affected Battery Ammeter and will be noted on be placed on affected Battery Ammeter and will be noted on be placed in a prominent be placed on Voltmeter and will be noted on be placed on Voltmeter and will be noted on be placed in a prominent be placed in a prominent

69 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ELECTRICAL POWER 8. Electrical Power System EICAS Displays MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 1) L Gen Voltmeter C 1 0 May be inoperative provided the associated frequency and loadmeter are operative. 2) L Gen Frequency Meter C 1 0 May be inoperative provided the associated voltmeter and loadmeter are operative. 3) L Gen Loadmeter C 1 0 May be inoperative provided the associated voltmeter and frequency meter are operative. 4) R Gen Voltmeter C 1 0 May be inoperative provided the associated frequency and loadmeter are operative. 5) R Gen Frequency Meter (continued) C 1 0 May be inoperative provided the associated voltmeter and loadmeter are operative. be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent

70 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ELECTRICAL POWER 8. Electrical Power System EICAS Displays (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 6) R Gen Loadmeter C 1 0 May be inoperative provided the associated voltmeter and frequency meter are operative. 7) APU Voltmeter C 1 0 May be inoperative provided the associated frequency meter and loadmeter are operative. 8) APU Frequency Meter C 1 0 May be inoperative provided the associated voltmeter and loadmeter are operative. 9) APU Loadmeter C 1 0 May be inoperative provided the associated voltmeter and frequency meter are operative. 10) Ext AC Pwr Voltmeter (continued) C 1 0 May be inoperative provided the associated frequency meter and loadmeter are operative. D 1 0 May be inoperative provided the associated external AC power is not used. be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent

71 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ELECTRICAL POWER 8. Electrical Power System EICAS Displays (cont d) 11) Ext AC Pwr Frequency Meter MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 1 0 May be inoperative provided the associated voltmeter and loadmeter are operative. D 1 0 May be inoperative provided the associated external AC power is not used. 12) Ext AC Loadmeter C 1 0 May be inoperative provided the associated frequency and voltmeter are operative. 13) Main, Essential and AUX TRU Voltmeters (continued) D 1 0 May be inoperative provided the associated external AC power is not used. C 5 0 May be inoperative provided the associated loadmeters are operative. be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent

72 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-8 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ELECTRICAL POWER 8. Electrical Power System EICAS Displays (cont d) 14) Main, Essential and AUX TRU Loadmeters (GV-SP, GIV-X) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: (GV) C ) Ext DC Pwr Voltmeter 16) Ext DC Pwr Loadmeter C 5 0 May be inoperative provided the associated voltmeters are operative. May be inoperative provided the associated: a) Voltmeters are operative, and b) Aeroplane is operated in accordance with AFM Limitations. C 1 0 May be inoperative provided the associated loadmeter is operative. D 1 0 May be inoperative provided the associated external DC power is not used. C 1 0 May be inoperative provided the associated voltmeter is operative. D 1 0 May be inoperative provided the associated external DC power is not used. be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent be placed in a prominent

73 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 24-9 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 24. ELECTRICAL POWER 9. Master Power Switch Lights (Left, Right, APU, EXT) 10. Battery Temperature *** Indicating System 11. Standby Electrical System MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 4 3 May be inoperative provided associated AC loadmeter and voltmeter are operative and selected for monitoring on the AC Synoptic. be placed on affected Master Power Switch and will be noted on D 1 0 C 1 0 May be inoperative provided both engine driven generators and APU generator are operative. be placed adjacent to Standby Electrical Master System and will be noted on 12. External Power System D Low Battery Power *** Audible Warning System (Sonalert) 14. Ground Service Bus System D 1 0 D 1 0

74 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 24. ELECTRICAL POWER Hz/60Hz AC *** Electrical Power Systems 16. IRU Back Up Batteries (GV) (continued) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D - 0 (M)(O) May be inoperative provided affected circuit breaker is pulled and collared. A 2 0 May be inoperative provided: a) Aeroplane is operated in day VMC conditions, and b) Repairs are made within one (1) flight day. A 2 0 May be inoperative provided: a) All other components of the Electrical Power system are operative, and b) Repairs are made within one (1) flight day. Maintenance will pull and collar affected circuit breaker. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will brief the passengers on the items that are inoperative with the failure of the power source for cabin entertainment.

75 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 24. ELECTRICAL POWER 16. IRU Back Up Batteries (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 (GV-SP, GIV-X) B 2 1 (M) May be inoperative provided that the affected battery is located in the #2 or #3 IRU back up battery position. A 2 0 May be inoperative provided: a) Aeroplane is operated in day VMC conditions, and b) Repairs are made within one (1) flight day. NOTE: EICAS message IRU Sec Pwr Fail will be displayed. A 2 0 May be inoperative provided: a) All other components of the Electrical Power system are operative, and b) Repairs are made within one (1) flight day. Maintenance will move affected battery to the #2 or #3 position.

76 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 25. EQUIPMENT/FURNISHINGS MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ Overwater Equipment D - - As required by regulations. If installed, an Inoperative Placard will be placed in a prominent position to be seen by flight crew and will be noted on 2. Passenger Seats D - - May be inoperative provided: a) Seat does not block an Emergency Exit, b) Seat does not restrict any passenger from access to the main aeroplane aisle, and c) The affected seat(s) are blocked and placarded "DO NOT OCCUPY". (continued) NOTE 1: A seat with an inoperative seat belt is considered inoperative. NOTE 2: Inoperative seats do not affect the required number of Flight Attendants. NOTE 3: Affected seat(s) may include the seat(s) behind and/or adjacent outboard seats. A "Do Not Occupy" Placard will be placed on affected seat and will be noted on

77 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 25. EQUIPMENT/FURNISHINGS 2. Passenger Seats (cont d) 1) Recline Mechanism *** 2) Underseat Baggage Restraining Bars (continued) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D - - (M) May be inoperative and seat occupied provided seat back is secured in the full upright position. C - - May be inoperative and seat occupied provided seat back is immovable in full upright position. D - - (O) May be inoperative provided: a) Baggage is not stowed under seat with inoperative restraining bar, b) Associated seat is placarded DO NOT STOW BAGGAGE UNDER THIS SEAT, and c) Procedures are established to alert Cabin Crew of inoperative restraining bars. Maintenance will ensure seat back is secured in full upright position. A "Do Not Occupy" Placard will be placed of affected seat not secured in up-right position and will be noted on A "Do Not Occupy" Placard will be placed of affected seat not secured in up-right position and will be noted on Flight crew will advise cabin crew which seat is affected and mark this seat with a tag or placard visible to crew and passengers. A "Do Not Stow Baggage Under This Seat" Placard will be placed of affected seat and will be noted on

78 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 2. Passenger Seats (cont d) 3) Armrests a) Armrests with Recline Mechanism b) Armrest without Recline Mechanism *** 4) Swivel Mechanism (continued) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D - - (M) May be inoperative or missing and seat occupied provided: a) Armrest does not block an Emergency Exit, b) Armrest does not restrict any passenger from access to the main aeroplane aisle, and c) If armrest is missing, seat is secured in the full upright position. D - - May be inoperative or missing and seat occupied provided: a) Armrest does not block an Emergency Exit, and b) Armrest does not restrict any passenger from access to the main aeroplane aisle. C - - May be inoperative and seat occupied provided: a) Associated seat does not block an Emergency Exit, b) Associated seat does not restrict any passenger from access to the main aeroplane aisle, and c) Associated seat remains in takeoff position. Maintenance will ensure seat is secured in the full upright position if armrest is missing. A "Do Not Occupy" Placard will be placed of affected seat not secured in up-right position and will be noted on A "Do Not Occupy" Placard will be placed of affected seat and will be noted on A Swivel Mechanism Inoperative Placard will be placed on affected seat, associated seat will remain in takeoff position and will be noted on

79 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 2. Passenger Seats (cont d) *** 5) Divan High Backs ***6) Electrical / Electronic Systems / Components 3. Crewmember Shoulder Harnesses MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C - - May be inoperative and seat occupied provided: a) Associated seat does not block an Emergency Exit, b) Associated seat does not restrict any passenger from access to the main aeroplane aisle, and c) Associated seat remains in takeoff position. C - - (M) May be inoperative and seat occupied provided associated component(s) is deactivated. B - - Any in excess of those required by flight deck crewmembers (including official observer in observer's seat) may be inoperative. 4. Observer Seat D 1 0 May be inoperative provided seat is not required and is correctly stowed. Maintenance will disconnect bag and stow the electrical connectors. Flight crew may accomplish this task if properly qualified and authorised. A "Do Not Occupy" Placard will be placed on affected seat and will be noted on

80 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 5. Megaphones *** 6. Flotation Devices 1) Life Rafts *** (continued) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D - - Any in excess of those required may be inoperative or missing provided: a) Inoperative megaphone is removed from passenger cabin, b) Associated placard is removed or obscured, and c) Required distribution is maintained. D - - (O) May be inoperative or missing provided: a) Overwater flights beyond 30 minutes at normal cruising speed or 50 NM away from land, whichever is the lesser are prohibited, and b) Procedures are established and used to alert crew members of inoperative or missing equipment. C - - (M)(O) Any in excess of those required for the intended flight may be inoperative or missing for flights over water provided: a) Required distribution is maintained, b) Inoperative lift raft and its installed location are placarded inoperative, c) When practical, the inoperative life raft is secured out of sight, and d) Procedures are established and used to alert crew members of inoperative or missing equipment. Maintenance will provide instructions to placard the inoperative life raft and its installed location and secure life raft in an out of sight location. Flight crew shall plan the flight appropriately to avoid overwater flights and alert crew members of inoperative or missing equipment Flight crew shall plan the flight appropriately to avoid overwater flights and alert crew members of inoperative or missing equipment be placed in a prominent be placed in a prominent

81 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 6. Flotation Devices (cont d) 2) Life Jackets D - - (M) Any in excess of those provided may be missing or inoperative provided: a) Inoperative life jacket is placarded inoperative, removed from the installed location and placed out of sight so it cannot be mistaken for a functional unit, and b) Required distribution of operative life jackets is maintained. 7. "Fasten Seat BeltWhile *** Seated Signs or Placards C - - One or more signs or placards may be illegible or missing provided a legible sign or placard is readable from each occupied passenger seat. Maintenance will provide instructions to placard the inoperative life jacket and its installed location and secure life raft in an out of sight location. be placed in a prominent A "Do Not Occupy" Placard will be placed on any affected seat from which signs are not readable and will be noted on

82 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 8. Storage Bin(s)/Cabin *** and Galley Storage Compartment/Closets (continued) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C - - (M) May be inoperative provided: a) Procedures are established to secure the affected bin, compartment or closet in the closed position, b) Associated bin, compartment or closet is prominently placarded DO NOT USE, c) Any emergency equipment located in affected compartment is considered inoperative, and d) Affected bin, compartment or closet is not used for storage of any items except for those permanently affixed. NOTE: For overhead bins, if no partitions are installed, the entire overhead bin is considered inoperative. Maintenance will verify that no emergency equipment is stored in the compartment, secure the compartment CLOSED and placard it against use for storage of any equipment. be placed on affected Storage Bin(s)/Cabin and Galley Storage Compartment/Closets and will be noted on

83 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-8 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 8. Storage Bin(s)/Cabin *** and Galley Storage Compartment/Closets (cont d) *** 1) Storage Compartment Key Locks MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C - - (M)(O) May be inoperative provided: a) For non-retractable doors, affected door is removed, b) For retractable doors, affected door is removed or secured in the retracted (fully open) position, c) Affected bin, compartment or closet is not used for storage of any items, except those permanently affixed, d) Affected bin, compartment or closet is prominently placarded DO NOT USE, e) Procedures are established and used to alert crew members and passengers of inoperative bins, compartments or closets, and f) Passengers are briefed that associated bin, compartment or closet is not used. NOTE 1: For overhead bins, if no partitions are installed, the entire overhead bin is considered inoperative. NOTE 2: Any emergency equipment located in the affected bin, compartment or closet (permanently affixed) is available for use. D - 0 (M) May be inoperative in unlocked position provided doors can be secured by other means. Maintenance will verify that no emergency equipment is stored in the compartment, secure the compartment CLOSED and placard it against use for storage of any equipment. Maintenance will verify that no emergency equipment is stored in the compartment, secure the compartment CLOSED and placard it against use for storage of any equipment. Flight crew will ensure passengers are briefed that bin or compartment is not used. be placed on affected Storage Bin(s)/Cabin and Galley Storage Compartment/Closets and will be noted on be placed on affected Storage Bin(s)/Cabin and Galley Storage Compartment/Closets Lock and will be noted on

84 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 25-9 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 25. EQUIPMENT/FURNISHINGS 9. Cargo Restraint *** Systems MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D - - (M) May be inoperative, or missing provided acceptable cargo loading limits from the approved appropriate model Gulfstream Cargo Loading Manual, or Weight & Balance Document are observed. Maintenance will ensure acceptable cargo loading limits from the approved appropriate model Gulfstream Cargo Loading Manual, or Weight & Balance Document are observed. Flight crew may accomplish this task if properly qualified and authorised. C - - May be inoperative, or missing provided cargo compartment remains empty.

85 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 25. EQUIPMENT/FURNISHINGS 10. Non-Required Cabin *** Crew Seat(s) 11. Galley/Cabin Waste Receptacles Access Doors/Covers MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C - 0 (M)(O) Seat or seat assembly may be inoperative provided: a) Inopertive seat or seat assembly is not occupied, b) Alternate procedures are established and used for displaced cabin crew, c) Folding type seat is stowed or secured in the retracted position, d) Where passenger seat is assigned to the displaced cabin crew it is placarded FOR CABIN CREW USE ONLY. NOTE: A seat position with an inoperative or missing seat belt harness is considered inoperative. C - - (M)(O) May be inoperative provided: a) The container is empty and the access is secured to prevent waste introduction into the compartment, and b) Procedures are established to ensure that sufficient galley waste receptacles are available to accommodate all waste that may be generated on a flight. Maintenance will ensure: a) Folding type seat is stowed or sedured in the retracted position, b) Passenger seat assigned to flight attendant is placarded FOR FLIGHT ATTENDANT ONLY and c) Repairs are made within two (2) flight days. Maintenance will ensure container is empty and the access is secured to prevent waste introduction into the compartment. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will ensure: a) Affected seat or seat assembly is not occupied, b) Flight attendant displaced by inoperative seat occupies the passenger seat most accessible to the inoperative seat, and c) Alternate procedures are established and used as published in crewmember manuals. Flight crew will ensure procedures are established to ensure that sufficient galley waste receptacles (trash bags are considered receptacles) are available to accommodate all waste that may be generated. be placed on affected Flight Attendant Seat and will be noted on be placed on affected Galley / Cabin Waste Receptacles Access Doors/Covers and will be noted on

86 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 12. Exterior Lavatory *** Door Ashtrays 1) Aeroplanes with multiple exterior lavatory door ashtrays installed 2) Aeroplanes with only one exterior lavatory door ashtray installed 13. External Camera *** System MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: A - 0 One or more may be inoperative or missing provided repairs are made within three consecutive calendar days. A - - One or more may be inoperative or missing provided: a) One operative exterior lavatory door ashtray can be readily seen and accessed from the affected lavatory door, and b) Repairs are made within ten consecutive calendar days. D - 0 (M)(O) One or more may be inoperative or missing provided: a) Affected lavatory door is locked closed and placarded to prohibit passengers entrance, and b) Affected lavatory is used only by crew members. A 1 0 May be missing or inoperative for three days. be placed on affected Exterior Lavatory Door Ashtray and will be noted on be placed on affected Exterior Lavatory Door Ashtray and will be noted on Maintenance will secure the door locked closed and placard it to prohibit passengers entrance. Flight crew will ensure passengers are briefed that lavatory is not to be used. be placed on affected Exterior Lavatory Door Ashtray and will be noted on be placed on affected Exterior Lavatory Door Ashtray and will be noted on D 1 0

87 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 14. Emergency Vision *** Assurance System (EVAS) STC No. SA00892LA 15. Pilot Seat(s) 1) Vertical Adjustment MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D - 0 May be inoperative provided the system is deactivated or the EVAS system is removed from the aeroplane. B - - (M)(O) May be inoperative provided: a) Seat is secured at the individual crewmember s requirements, and b) Fore-aft adjustment is operative. 2) Armrest C - - (M)(O) May be inoperative provided: a) Affected armrest is in the upright position or removed, and b) Seat is acceptable to the affected crewmember. 3) Recline Adjustment B - - (M)(O) May be inoperative provided: a) Seat is secured at a position acceptable to the affected crewmember, and b) Seat is able to move full Fore-Aft on its track. 4) Lumbar Support C - - May be inoperative provided seat is acceptable to the affected crewmember. 5) Thigh Support C - - May be inoperative provided seat is acceptable to the affected crewmember. be placed on vertical adjustment handle and will be noted on Maintenance will secure seat as required by proviso a) and ensure that seat is able to move full fore and aft on its track. Maintenance will ensure armrest is in the up position or removed. Maintenance will secure seat as required by proviso a) and ensure that seat is able to move full fore and aft on its track. Flight crew will evaluate seat for suitability. Flight crew will evaluate seat for suitability. Flight crew will evaluate seat for suitability. be placed on vertical adjustment handle and will be noted on be placed on affected arm rest and will be noted on be placed on recline adjustment handle and will be noted on be placed on the pilots seat adjustment to lumbar support area and will be noted on be placed on the pilots seat adjustment to thigh support area and will be noted on

88 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 25. EQUIPMENT/FURNISHINGS 16. Rudder Pedal Adjustment 17. Cockpit Convenience Items MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 2 0 (M) May be inoperative provided: a) Adjustments can be secured in a position that suits individual pilot(s), and b) Position of pedal(s) permits normal full flight control movement. C - 0 NOTE: Items such as sunshades, cup holders, curtains, cushions, vent knobs, gaspers, upholstery / trim, goggles stowage bags, side panel holders, side view mirrors, foot rests, foot warmer handles and vents, and yoke clips may be inoperative or missing. 18. Keyed Locks D - 0 May be inoperative provided the associated access panel, door, compartment, or cap is verified secure before each departure. Maintenance will ensure adjustments can be secured in a position that suits individual pilot(s) requirements and position of pedal(s) permits normal full flight control movement. Flight crew may perform procedures if maintenance is not available. be on the rudder pedal adjustment handle and will be noted on 19. Aeroplane Ladders C - 0 (O) May be inoperative or removed. Flight crew will ensure inoperative ladder is secured or removed prior to each departure. 1) Ladder Hardware (Pit Pins, Lanyards, etc.) D - 0

89 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 25. EQUIPMENT/FURNISHINGS 20. Baggage Compartment *** Shelves *** 1) Shelf Stowage Straps *** 2) Shelf Support Straps 21. Crewmember Torches Holder Assemblies (including torch) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D - 0 May be inoperative or removed provided the shelves remain in the down position. D - 0 May be inoperative or removed provided the shelves remain in the stowed (up) position and are not used. C - 0 May be inoperative or missing provided crewmember has a torch of equivalent characteristics readily available.

90 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 25. EQUIPMENT/FURNISHINGS 22. Automatic External *** Defibrillator (AED) and/or Associated Equipment 23. Emergency Medical *** Kit (EMK) and/or Associated Equipment MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 A - 0 (O) May be incomplete, missing or inoperative provided: a) AED is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs are made within three (3) flight cycles. D - - Any in excess of those required by Operating Requirements may be incomplete, missing, or inoperative. A - 0 (O) May be incomplete, missing or inoperative provided: a) EMK is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within two (2) calendar days. D - - Any in excess of those required may be incomplete, missing or inoperative. Flight crew will ensure AED unit is placarded DO NOT USE THIS UNIT. SOME REQUIRED ITEMS MAY BE MISSING., and repairs are made within three (3) flight cycles. be will be placed on Automatic External Defibrillator and/or Associated Equipment and will be noted on be will be placed on Automatic External Defibrillator and/or Associated Equipment and will be noted on Flight crew will ensure EMK unit is placarded DO NOT USE THIS UNIT. SOME REQUIRED ITEMS MAY BE MISSING., and repairs are made within two (2) calendar days. be will be placed on Emergency Medical Kit (EMK) and/or Associated Equipment and will be noted on be will be placed on Emergency Medical Kit (EMK) and/or Associated Equipment and will be noted on

91 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 24. First Aid Kit (FAK) and/or Associated Equipment 25. Flight Crew Sleeping *** Facilities Crew Seat (includes crew seat recline mechanism, berthing mechanism, armrests, swivel mechanism, and electrical/electronic systems/components) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: A - - (O) If more than one is required, only one of the required first aid kits may be incomplete, missing or inoperative provided: a) FAK is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within two (2) flight cycles. D - - Any in excess of those required may be incomplete, missing or inoperative. C - 0 (M) (O) May be inoperative provided: a) Crew seat is secured in a position acceptable to the crewmember(s) who will occupy the crew rest area, and b) Crew rest area is used in accordance with the operating requirements. D - 0 (O) May be inoperative provided: a) Crew seat is not occupied, and b) Crew Rest is placarded INOPERATIVE DO NOT USE. Flight crew will ensure FAK unit is placarded DO NOT USE THIS UNIT. SOME REQUIRED ITEMS MAY BE MISSING., and repairs are made within two (2) flight cycles. be will be placed on First Aid Kit and/or Associated Equipment and will be noted on be will be placed on First Aid Kit and/or Associated Equipment and will be noted on Maintenance will ensure seat / bunk, and all its mechanisms and components, are secured to the individual creewmembers requirements. Flight crew will evaluate seat to ensure it is acceptable for resting. Flight crew will ensure crew rest facility is placarded INOPERATIVE-DO NOT USE.

92 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 26. Passenger Convenience Items 27. Cabin Management System MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D - 0 NOTE 1: Passenger convenience items are those related to passenger convenience, comfort or entertainment, such as, but not limited to galley equipment, movie equipment, ashtrays, stereo equipment, and overhead reading lamps. Items addressed elsewhere in this document shall not be included. NOTE 2: Lavatory door ashtrays are not considered convenience items. D 1 0 *** 1) Cabin Power Bus D 1 0 *** 2) Advanced Cabin Server *** 3) GCMS Controllers (continued) D 2 0 D 2 0

93 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: EQUIPMENT/FURNISHINGS 27. Cabin Management System (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: *** 4) I/O Concentrators D 2 0 *** 5) Switching Nodes D 25 0 *** 6) AVDS Nodes D 4 0 *** 7) Galley Touch Screen *** 8) Vestibule Touch Screen D 1 0 D 1 0 *** 9) Maintenance Server D 1 0

94 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 26-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 26. FIRE PROTECTION 1. Portable Fire Extinguishers D - - Any in excess of those required by Operating Requirements may be inoperative or missing provided: a) Inoperative fire extinguisher is tagged inoperative, removed from the installed location, and placed out of sight so it cannot be mistaken for a functional unit, and b) Required distribution is maintained. If installed, an Inoperative Placard will be placed on Pressure Charge Gauge of affected extinguisher and will be noted on 2. Wing Overheat Warning Systems 3. APU Fire Detection System C 2 0 Except for ER operations, may be inoperative provided: a) Wing Anti-ice is not used, and b) Aeroplane is not operated in known or forecast icing conditions. C 1 0 (M) Except for ER operations, may be inoperative provided: a) APU is not used, and b) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. be placed adjacent to affected Wing Anti-Ice Switch and will be noted on Maintenance will ensure APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. be placed on APU "MASTER" Switch and will be noted on

95 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 26-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FIRE PROTECTION 4. Rear Baggage Compartment Smoke Detector Systems C - 0 May be inoperative provided: a) Internal baggage door remains OPEN, and b) Aeroplane is operated at or below FL Lavatory Smoke *** Detection Systems C - 0 May be inoperative provided: a) Rear baggage compartment is not used, b) Internal baggage door remains CLOSED, c) Flight crew investigates baggage compartment for possible fire in the event the "BAG EER HOT" message displays, and d) Aeroplane is operated in accordance with AFM Limitations. C - - (M)(O) For each lavatory, the lavatory smoke detection system may be inoperative provided: a) Lavatory waste receptacle is empty, b) Associated lavatory door is LOCKED, CLOSED and placarded, "INOPERATIVE - DO NOT ENTER", and c) Lavatory is used only by crewmembers. NOTE 1: These provisos are not intended to prohibit lavatory use or inspections by crewmembers. NOTE 2: Lavatory smoke detection system is not required for all-cargo operations. Maintenance will ensure Lavatory Smoke Detector CB is pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will inspect lavatory to ensure Lavatory Waste Receptacle is empty and Lavatory Door is LOCKED CLOSED. In addition, flight crew will ensure Lavatory is NOT used for any purpose. be placed on Lavatory Door stating "Inoperative - Do Not Enter" and will be noted on NOTE: These provisos are not intended to prohibit lavatory use or inspections by crewmembers. In addition, Lavatory Smoke Detection System is not required for all -cargo operations.

96 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 26-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FIRE PROTECTION 6. Lavatory Fire *** Extinguisher Systems 7. Galley Smoke *** Detection Systems C - - For each lavatory, the lavatory fire extinguisher system may be inoperative provided Lavatory Smoke Detector system is operative. C - - (M)(O) For each lavatory, the lavatory fire extinguisher system may be inoperative provided: a) Lavatory waste receptacle is empty, b) Associated lavatory door is LOCKED, CLOSED and placarded, "INOPERATIVE - DO NOT ENTER", and c) Lavatory is used only by crewmembers. NOTE 1: These provisos are not intended to prohibit lavatory use or inspections by crewmembers. NOTE 2: A Lavatory Fire Extinguisher System is not required for all-cargo operations. be placed on the Lavatory Fire Extinguisher and will be noted on Maintenance will verify Lavatory Waste Receptacle is empty. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will inspect lavatory to ensure Lavatory Waste Receptacle is empty and Lavatory Door is LOCKED CLOSED. In addition, flight crew will ensure Lavatory is NOT used for any purpose. be placed on Lavatory Door stating "Inoperative Do Not Enter" and will be noted on D - 0 be placed on Galley Smoke Detector and will be noted on

97 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 26-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FIRE PROTECTION 8. Galley Fire *** Extinguishing Systems D - 0 be placed on Galley Fire Extinguisher and will be noted on 9. Engine Fire Detection Systems C 2 1 Except for ER opertions, one complete loop (A or B) may be inoperative provided the Fault Switch/ Light is pressed to isolate the faulty loop and illuminate the OFF portion of the switch light. An Inoperative Placard is placed next to either A or B Switch/Light and will be noted on 10. Flame Detectors *** 11. Electronic Equipment Rack Overheat Warning System D - 0 C Passenger *** Compartment Closet Smoke Detectors D - 0 May be inoperative provided door remains OPEN for visual check from crew stations. be placed on Passenger Compartment Closet Smoke Detectors and will be noted on

98 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 26-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 26. FIRE PROTECTION 13. Entranceway Baggage *** Compartment Smoke Detectors 14. Cargo Compartment *** 1) Smoke Detection- Systems *** 2) Fire Suppression Systems D - - May be inoperative provided door remains OPEN for visual check from crew stations. C - 0 (O) May be inoperative provided procedures are established and used to ensure the associated compartment or zone remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or fly away kits. NOTE: Operator MELs should define which items are approved for inclusion in the fly away kits, and which materials can be used as ballast. C - 0 (O) May be inoperative provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or fly away kits. NOTE: Operator MELs should define which items are approved for inclusion in the fly away kits, and which materials can be used as ballast. be placed on Entranceway Baggage Compartment Smoke Detectors and will be noted on Flight crew will verify that cargo compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast, and/or fly away kits. Flight crew will verify that cargo compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast, and/or fly away kits.

99 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 26-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FIRE PROTECTION 15. APU Fire Bottle *** C 1 0 (M)(O) Except for ER operations, may be inoperative provided: a) APU is considered inoperative, b) Both engine driven generators are operative, c) Standby electrical system is operative, and d) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Maintenance will pull and collar APU CONT #1 and APU CONT #2 circuit breakers. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will ensure: a) Maintenance procedures are accomplished if maintenance personnel are not available. AFM Normal Procedures. b) Both Engine Generators are operative. c) Standby Electrical Power System is operative. AFM Emergency Procedures. be placed on APU Fire Bottle and will be noted on

100 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 27-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 27. FLIGHT CONTROLS 1. Rudder Limit Indication System 2. Single Rudder Indication System 3. Automatic Ground Spoiler System C 1 0 May be inoperative provided Single Rudder Indication System is operative. C 1 0 May be inoperative provided Rudder Limit Indication System is operative. C 1 0 (O) May be inoperative provided aeroplane is operated in accordance with AFM Limitations. Flight crew will ensure aeroplane is operated in accordance with AFM, Section 1, Limitations, and Automatic Ground Spoilers. (On dry and wet runways (less than 3mm of standing water) takeoff is permitted with Automatic Ground Spoilers inoperative provided the Anti-Skid is operative, 20 o flaps are used and the Cowl and Wing Anti-Ice systems are not used. Takeoff with Automatic Ground Spoilers inoperative is not permitted on contaminated runways under any circumstances.)

101 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 27-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FLIGHT CONTROLS 4. Electric Elevator Trim System 5. Control Wheel Elevator Trim Switches C 1 0 (O) May be inoperative provided: a) Electric Elevator Trim remains OFF, b) Both Flap/Stabilizer Control Channels are operative, and c) Aeroplane is operated in accordance with AFM Limitations. C 2 1 (O) May be inoperative provided pilot flying has operative switch. Flight crew will ensure Electric Pitch Trim remains "OFF", both Flap/ Stabilizer Control Channels are operative (no messages on CAS), and aeroplane is operated in accordance with AFM, Section 1, Limitations, Airspeed Limitations. (Maximum Operating Limit Speed is 0.80 Mt.) In the event that the operative Elevator Trim Switch fails after dispatch, the crew shall comply with the Jammed Stabilizer procedure in Section 3 Abnormal Procedures of the applicable AFM. Maximum flap selection is 20 degrees during the approach and landing. be placed next to Pitch Trim Switch and will be noted on be placed in a prominent 6. Flap/Stabilizer Control Channels 7. Single Speed Brake Indication System B 2 1 Channel may be inoperative provided: a) Electric Pitch Trim System is operative, and b) Alternate control is verified operative before each departure. C 1 0 May be inoperative provided Single Rudder Indication System is operative. None required be placed in a prominent None required be placed in a prominent

102 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 27-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FLIGHT CONTROLS 8. Elevator Trim *** Actuator Heater Systems 9. Aileron Trim *** Actuator Heater 10. Autopilot Elevator Servos (GV-SP, GIV-X) 11. Autopilot Pitch Trim Servos (GV-SP, GIV-X) 12. Autopilot Aileron Servos (GV-SP, GIV-X) B 2 0 (M)(O) May be inoperative provided affected circuit breaker(s) are pulled and collared. C 1 0 (M)(O) May be inoperative provided affected circuit breaker(s) are pulled and collared. C 2 1 (M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared. C 2 1 (M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared. C 2 1 (M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared. Maintenance will ensure affected circuit breaker(s) are pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will ensure affected circuit breaker(s) are pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will ensure inoperative servo circuit breaker(s) is pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will ensure inoperative servo circuit breaker(s) is pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will ensure inoperative servo circuit breaker(s) is pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will ensure maintenance procedures are accomplished if maintenance personnel are not available. Flight crew will ensure maintenance procedures are accomplished if maintenance personnel are not available. be placed next to Elevator Trim Actuator Switch and will be noted on be placed next to Aileron Trim Wheel and will be noted on be placed in a prominent be placed in a prominent be placed in a prominent

103 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 27-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FLIGHT CONTROLS 13. Autopilot Yaw Damper Servos (GV-SP, GIV-X) 14. Stall Barrier Systems C 2 1 (M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared. A 2 1 (M)(O) May be inoperative provided: a) Angle of Attack indication is available on both PFD s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled, and d) Repairs are made within two (2) flight days. Maintenance will ensure inoperative servo circuit breaker(s) is pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will pull and collar the circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be crossreferenced to Normalized Angle of Attack to 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear at the departure of destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist or consider deviation to an alternate airport in the approach and landing case. be placed in a prominent be placed in a prominent

104 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 27-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: FLIGHT CONTROLS 15. Flight Control Synoptic Display (GV) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 1 0 May be inoperative provided the affected control surface is visually checked for full, free and correct movement prior to each flight. (GV-SP, GIV-X) C - 0 May be inoperative provided the affected control surface is visually checked for full, free and correct movement prior to each flight. 16. Gust Lock C 1 0 (O) May be inoperative provided flight controls are secured in an alternate manner in accordance with GAC-OIS-14. C 1 0 (O) May be inoperative provided aeroplane is parked in sheltered area unaffected by atmospheric conditions. be placed in a prominent be placed in a prominent Flight crew will secure affected surfaces by using rope or some other means to secure the rudder pedals and control yoke from moving between flights. Flight crew will park the airplane in a sheltered area (hangar) or determine via weather forecasts that the rudder, elevator and ailerons won t be exposed to windy conditions. be placed in a prominent be placed in a prominent

105 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 28-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 28. FUEL 1. Fuel Tank Temperature Systems (GV, GV-SP) Fuel Tank Temperature System (GIV-X) 2. EICAS or Standby RFMU (GV) / MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems (continued ) C 2 0 (O) May be inoperative provided: a) Total Air Temperature is used as an indication of fuel temperature, and b) Aeroplane is operated in accordance with AFM Limitations. C 1 0 (O) May be inoperative provided: a) Total Air Temperature is used as an indication of fuel temperautre, and b) Aeroplane is operated in accordance with AFM Linitations. C 2 1 (M)(O) May be inoperative provided a) Associated Standby Fuel Quantity Indicating System or EICAS Fuel Quantity Indicating System is operative, and b) Either the primary or the standby fuel quantity indication displays Left and Right Fuel Quantity. Maintenance will ensure tanks are filled using Standby Fuel Quantity Indicating System or EICAS Fuel Quantity Indicating System. Flight crew will ensure Total Air Temperature (TAT) is used as indication of fuel temperature and aeroplane is operated in accordance with AFM, Section 1, Limitations, Powerplant EICAS Indications. Flight crew will ensure Total Air Temperature (TAT) is used as indication of fuel temperature and aeroplane is operated in accordance with AFM, Section 1, Limitations, Powerplant EICAS Indications. Flight crew will ensure associated Standby Fuel Quantity Indicating System or EICAS Fuel Quantity Indicating System is operative.

106 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 28-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 28. FUEL 2. EICAS or Standby RFMU (GV) / MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems (cont d) C 2 1 (M)(O) Except for ER operations, either Left or Right Fuel Quantity display may be inoperative provided: a) Both tanks are completely filled using overwing refueling, b) Both fuel flow meters are operative, c) After takeoff, power is set by matching fuel flow indications on both engines, and d) Flight crew maintains a log of fuel burned. NOTE 1: Failure to display either Left or Right Fuel Quantity exists in both the primary and secondary fuel quantity indications. NOTE 2: Total fuel indication will be invalid with an inoperative indicator. C 2 1 (M)(O) Except for ER operations, either Left or Right Fuel Quantity display may be inoperative provided: a) Affected tank is defueled before each refueling, b) Affected tank is fueled with a known quantity of fuel, c) Both fuel flow meters are operative, d) After takeoff, power is set by matching fuel flow indications on both engines, and e) Flight crew maintains a log of fuel burned. NOTE 1: Failure to display either Left or Right Fuel Quantity exists in both the primary and secondary fuel quantity indications. NOTE 2: Total fuel indication will be invalid with an inoperative indicator. Maintenance will ensure BOTH tanks are completely filled using overwing method of refueling. NOTE: Do not pull Fuel Qty circuit breaker as this disables Fuel Level Low caution message. Maintenance will Defuel affected tank before each refueling and refuel it with Known quantity of fuel. Flight crew will ensure: a) Both Fuel Flow Indicating Systems are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator. Flight crew will ensure: a) Both fuel flow meters are operative, b) After takeoff, power is set by matching fuel flow indications on both engines, and c) A log of fuel burned is maintained. NOTE: Total fuel indication will be INVALID with inoperative indicator.

107 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 28-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 28. FUEL 3. Fuel Low Quantity Warning Systems MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 2 0 (O) May be inoperative provided: a) Both Fuel Quantity Indicating Systems are operative, b) All Fuel Boost Pumps are operative, and c) Fuel Crossflow Valve is OPENED when either wing tank contains 2,000 pounds or less fuel. 4. Fuel Boost Pumps C 4 3 (O) Except for ER operations, may be inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, and d) Aeroplane is operated in accordance with AFM Limitations. Flight crew will ensure: a) BOTH Fuel Quantity Indicating Systems and all Fuel Boost Pumps are operative. (AFM, Section 2, Normal Procedures, Before Starting Engines, Normal Engine Ground Start and After Starting Engines) b) Fuel Crossflow Valve is OPENED when either wing tank contains 2,000 pounds or less fuel. Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative. AFM, Section 2, Normal Procedures, Before Starting Engines. b) BOTH Fuel Low Quantity Warning Systems are operative. AFM, Section 2, Normal Procedures, Before Starting Engines. c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure. be placed in a prominent be placed on Affected Fuel Boost Pump "ON/OFF" Switch and will be noted on

108 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 28-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FUEL 5. Fuel Intertank Valve 6. Heated Fuel Return System (HFRS) (GV, GV-SP) 7. Fuel Boost Pump Warning Systems C 1 0 (M) Except for ER operations, may be inoperative provided: a) All Fuel Boost Pumps are operative, b) Fuel Crossflow Valve is operative, c) Fuel Quantity Indicating System is operative, and d) Intertank Valve is verified CLOSED and electrically deactivated. NOTE: With Fuel Intertank Valve CLOSED and fuel temperature below 0 degrees C, fuel balancing capabilities may be affected. C 2 0 May be inoperative provided: a) Flight crew monitors fuel tank temperature, and b) Aeroplane is operated in accordance with AFM Limitations. C 4 3 (O) Except for ER operations, may be inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, and c) Aeroplane is operated in accordance with AFM Limitations. Maintenance will deactivate the intertank valve by pulling and collaring appropriate Fuel Intertank circuit breaker. Flight crew may accomplish this task if properly qualified and authorised. be placed on Fuel Intertank Valve Switch and will be noted on be placed in a prominent The flight crew will ensure the Fuel Crossflow Valve and Fuel Intertank is operative; AFM, Section 2, Normal Procedures, Before Starting Engines and Fuel Synoptic and that AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure are complied with. be placed on affected Boost Pump Warning Annunciator and will be noted on

109 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 28-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FUEL 8. Fuel Crossflow Valve 1) Failed CLOSED C 1 0 (O) Except for ER operations, may be inoperative provided: a) All Fuel Boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative, d) Fuel Intertank Valve is OPEN when either wing tank contains 2,000 pounds or less fuel, and e) Aeroplane is operated in accordance with AFM Limitations. Flight crew will comply with provisos a), b) and c) using AFM Section 2, Normal Procedures and Fuel Synoptic. Flight crew will OPEN Fuel Intertank Valve when either wing tank contains 2000 lb or less fuel. Aeroplane is operated in accordance with AFM, Section 1, Limitations, Fuel Balance (1000 lb takeoff, 2000 lb enroute). be placed on Fuel Crossflow Valve Switch and will be noted on NOTE: Avoid uncoordinated maneuvers when Fuel Intertank Valve is OPEN. 2) Failed OPEN C 1 0 (O) Except for ER operations, may be inoperative provided: a) All Fuel Boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative, d) Aeroplane is operated in accordance with AFM Limitations, and e) Fuel tank temperature system must be operative. Flight crew will use Normal Procedures and Fuel Synoptic to ensure: a) All Fuel Boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative. d) Fuel tank temperature system is operative. be placed on Fuel Crossflow Valve Switch and will be noted on NOTE: Avoid uncoordinated maneuvers when Fuel Intertank Valve is OPEN.

110 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 28-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 28. FUEL 9. Pressure Fueling System (Single Point Refueling) 10. Ground Service Control Panel 11. Automatic Fueling System MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D 1 0 (M) May be inoperative provided procedures are established to deactivate Pressure Fueling System. Maintenance will ensure Pressure Fueling System is deactivated by Manually Closing Fuel Precheck Valves and pulling and collaring appropriate (Left or Right) Fueling Shutoff Valve CB. AMM, chapter Flight crew may perform maintenance function if maintenance is unavailable and flight crew is properly qualified and authorised. be placed on Pressure Refueling Port and between Left and Right Remote Fueling Shutoff Switches and will be noted on D 1 0 be placed on Ground Service Control Panel and will be noted on D 1 0 be placed on Automatic Fueling System and will be noted on 12. Fuel Cap Chains D - 0 be placed in a prominent

111 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 28-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ FUEL 13. Single Point Refueling Cap 14. Mid Wing Ejector *** (MWE) System (GV, GV-SP only) C 1 0 May be inoperative or missing provided the single point refueling receptacle is checked for leaks before every takeoff. C 2 0 (O) One or both may be inoperative provided the maximum fuel load for dispatch is limited to 9,000 lb per tank for a total fuel load of 18,000 lb. be placed in a prominent The flight crew shall ensure that the maximum fuel load is equal to or less than 9,000 lb per tank for a maximum total of 18,000 lb. be placed in a prominent C 2 0 (O) May be inoperative provided: a) Maximum zero fuel gross weight is limited to 52,000 lb, and b) Zero fuel gross weight forward center of gravity is limited to 37.5% MAC. The flight crew will ensure that the max zero fuel gross weight does not exceed 52,000 lb and that the center of gravity is not forward of 37.5% MAC. be placed in a prominent

112 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 29-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ HYDRAULIC POWER 1. Brake Accumulator Pressure Gauge (Nose Wheelwell) D 1 0 be placed on face of Accumulator Pressure Indicator and will be noted on 2. Auxiliary Hydraulic Pump Pressure Indication 3. Power Transfer Unit (PTU) Hydraulic Pressure Indication 4. PTU Hydraulic Pump (Auto Mode) 5. Auxiliary Hydraulic Pump (Auto Mode) C 1 0 May be inoperative provided cockpit Brake Accumulator Pressure Gauge is operative. C 1 0 (O) May be inoperative provided: a) Left Hydraulic Pressure Indication is operative, b) PTU Hydraulic system is operative, and c) Before left engine start, HMG operational check is performed. C 1 0 May be inoperative provided manual mode is verified to be operative before every flight. C 1 0 May be inoperative provided Auxiliary pump is selected ON for takeoff and landing. Flight crew will ensure Hydraulic Pressure Indication is operative and Power Transfer Unit operation is verified by performing successful flap operational test with only right engine running. NOTE: With right engine running, select PTU ON. Verify PTU pressure is present (3000 psi +300/-400). be placed in a prominent be placed on Power Transfer Unit Arm Switch and will be noted on be placed on Auxiliary Hydraulic Pump Arm Switch and will be noted on

113 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 29-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 29. HYDRAULIC POWER 6. Left Hydraulic System Quantity Gauge (Ground Service Control Panel - Aft Equipment Area) 7. Right Hydraulic System Quantity Gauge (Ground Service Control Panel - Aft Equipment Area) 8. Left Hydraulic System Quantity Indication (EICAS) 9. Right Hydraulic System Quantity Indication (EICAS) 10. Hydraulic Reservoir Temperature Sensors D 1 0 (O) May be inoperative provided quantity is checked by reservoir indicator or using hydraulic quantity indication on hydraulic synoptic before each departure. D 1 0 (O) May be inoperative provided quantity is checked by reservoir indicator or using hydraulic quantity indication on hydraulic synoptic before each departure. C 1 0 May be inoperative provided quantity is checked by reservoir indicator or Ground Service Control Panel Left Hydraulic Quantity gauges before each departure. C 1 0 May be inoperative provided quantity is checked by reservoir indicator or Ground Service Control Panel Right Hydraulic Quantity gauges before each departure. B 2 0 NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures. Flight crew will verify the hydraulic quantity at the reservoir or on hydraulic synoptic prior to every departure. Flight crew will verify the hydraulic quantity at the reservoir or on hydraulic synoptic prior to every departure. be placed on Ground Service Control Panel and will be noted on be placed on Ground Service Control Panel and will be noted on

114 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 29-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 29. HYDRAULIC POWER 11. Hydraulic Reservoir Replenishing System 12. Brake Accumulator Pressure Gauge (cockpit dial) 13. Brake Synoptic Page Accumulator Pressure Indication D 1 0 (M) May be inoperative provided hydraulic reservoirs are replenishs as needed using approved servicing techniques. C 1 0 May be inoperative provided the Brake Synoptic Page Accumulator Pressure Indication is operative. C 1 0 May be inoperative provided: a) Brake accumulator gauge in the nose wheelwell is operative and checked before each takeoff, and b) Auxiliary hydraulic pump is on and running for every takeoff and landing. C 1 0 May be inoperative provided the Brake Accumulator Pressure Gauge (cockpit dial) is operative. Aeroplane may continue in service provided maintenance personnel replenish hydraulic reservoirs as needed using approved servicing techniques. Reference AMM C 1 0 May be inoperative provided: a) Brake accumulator gauge in the nose wheelwell is operative and checked before each takeoff, and b) Auxiliary hydraulic pump is on and running for every takeoff and landing.

115 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 30-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 30. ICE and RAIN PROTECTION 1. Cowl Anti-Ice Pressure Indication Systems 2. Wing Anti-Ice Systems 1) Automatic Functions MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 B 2 0 Except for ER operations, may be inoperative provided both EICAS Cowl Anti-Ice Indications are operative. B 2 0 Except for ER operations, may be inoperative provided aeroplane is operated at greater than +10 deg. SAT. B 2 0 Except for ER operations, may be inoperative provided: a) Aeroplane is operated in VMC, and b) Aeroplane is not operated in visible moisture. C 2 0 Except for ER opertions, may be inoperative provided aeroplane is not operated in known or forecast icing conditions. C 2 0 May be inoperative provided aeroplane is operated in accordance with AFM Limitations. be placed in a prominent be placed in a prominent be placed in a prominent be placed on affected Wing Anti-Ice "OFF/AUTO/ ON" Switch and will be noted on Refer to AFM Section , , and

116 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 30-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 30. ICE and RAIN PROTECTION 3. Windshield Heat Systems 1) Windshield Heat Sensors 4. Side Window Heat Systems 1) Side Window Heat Sensors MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 2 1 Except for ER operations, one may be inoperative provided: a) Aeroplane is not operated in known or forecast icing conditions, and b) Both side window heat systems are operative. D 4 2 One sensor may be inoperative for each Windshield Heat System. C 2 1 May be inoperative provided aeroplane is not operated into known or forecast icing conditions. D 4 2 One Side Window Heat Sensor may be inoperative for each Side Window Heat System. NOTE: No further relief is permitted.

117 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 30-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ICE and RAIN PROTECTION 5. Anti-Ice Heater Switch Lights MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: B 4 0 (M)(O) May be inoperative provided all other elements of the anti-ice heater indicating system are verified to operate normally. Maintenance will check all other elements of Probe Heat Control Switch and ensure them to be functional. Refer to AMM chapter Flight crew will ensure all other elements of Probe Heat Indicating Switch are functioning normally, i.e. when pitot heat is selected ON, appropriate EICAS fail message extinguishes. be placed on Probe Heat Switch and will be noted on 6. Pitot Heaters (GV, GV-SP) B 4 3 (O) Except for ER operations, may be inoperative provided aeroplane is not operated in visible moisture or known or forecast icing conditions. Flight crew will select MADC sources that are different and not associated with failed pitot heater element. (GIV-X) B 3 2 (O) Except for ER operations, may be inoperative provided aeroplane is not operated in visible moisture or known or forecast icing conditions. Flight crew will select MADC sources that are different and not associated with failed pitot heater element. 7. Ice Detection Systems D 2 0 (O) May be inoperative provided alternate procedures are established and used to monitor for the presence of ice. NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available. Refer to AFM Section , , and Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and the SAT is +10 C or less. Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges.

118 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 30-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 30. ICE and RAIN PROTECTION 8. Cowl Anti-Ice Systems 1) Automatic Functions MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 2 0 (M) Except for ER operations, may be inoperative provided: a) Affected Valve(s) are verified CLOSED, b) The switch for the affected valve(s) is selected to the OFF position, and c) Aeroplane is not operated in known or forecast icing conditions. C 2 1 (M) May be inoperative provided: a) Affected Valve(s) is secured OPEN, b) All components of both HP Bleed Air Systems are operative, c) Both Environmental Control System (ECS) Packs are operative, d) Performance Computer is initialized with COWL ANTI-ICE selected ON for either takeoff or landing when COWL ANTI-ICE valve is pressurized, and e) Aeroplane is operated in accordance with AFM Limitations and Performance. C 2 0 May be inoperative provided aeroplane is operated in accordance with alternate AFM procedures. Maintenance will ensure affected Cowl Anti-Ice Valve(s) is/are verified closed IAW RR EMM, task # Flight crew may accomplish this task if properly qualified and authorised. Maintenance will ensure: a) BOTH HP Bleed Air Systems and BOTH Environmental Control System (ECS) Packs are operative. b) Select the affected Cowl Anti- Ice switch ON and ensure that the affected valve circuit breaker is pulled or in the OPEN position. AMM, chapter , and Flight crew may accomplish this task if properly qualified and authorised. be placed on or next to affected Cowl Anti-Ice Switch indicting valve position and will be noted on be placed on or next to affected Cowl Anti-Ice Switch indicting valve position and will be noted on

119 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 30-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 30. ICE and RAIN PROTECTION 9. Cowl Pressure Differential Indication System 10. Windshield Blower *** System 1) Windshield Surface Seal Protection Systems MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 May be inoperative provided Cowl Anti- Ice Pressure Indications are operative. D 1 0 (M) May be inoperative provided the Surface Seal coating has been checked to be servicable in accordance with the Maintenance Manual within the last 12 months or 500 flight hours whichever occurs first. D 1 0 (M) May be inoperative provided the Surface Seal coating is checked to be serviceable in accordance with the Maintenance Manual. D 1 0 May be inoperative provided there is no precipitation falling on the departure and arrival airport at the time of taxi, takeoff and landing. D 2 0 Both may be inoperative provided aeroplane is not operated in precipitation within 5 NM of the airport of takeoff or intended landing. Maintenance will verify that effectiveness of windshield coating is in accordance with AMM within the last 12 months or 500 flight hours. Maintenance will verify that effectiveness of windshield coating is in accordance with AMM.

120 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 30-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ICE and RAIN PROTECTION 11. Cabin Window Heat System a) Cabin Window Heating Elements MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D 1 0 (M) May be inoperative provided: a) Cabin Window Heat switch is selected OFF, and b) Cabin Window Heat System circuit breakers are pulled and collared. D - 0 (M) May be inoperative provided the associated Window Heat circuit breakers are pulled and collared. Maintenance will ensure: a) Cabin Window Heat switch is selected OFF, and b) Affected Cabin Window Heat System circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will pull and collar the affected cabin window heat system circuit breakers.

121 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 31-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: INDICATING / RECORDING MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: SYSTEMS 1. Clocks (Cockpit) D - 1 be placed on affected Clock face and will be noted on 2. Flight Data Recorder *** (FDR) 1) (FDR) A - 0 One or more may be inoperative provided: a) Aeroplane does not exceed 8 further consecutive flights with flight data recorder unserviceable, b) Not more than 72 hours have elapsed since flight data recorder was found to be unserviceable, and c) Any cockpit voice recorder required to be carried is operative. (continued) be placed on FDR Control Panel and will be noted on

122 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 31-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: INDICATING / RECORDING SYSTEMS 2. Flight Data Recorder *** (FDR) (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 1) (FDR) NOTE 1: Flight data recorder is considered to be inoperative when any of the following conditions exist: a) Loss of flight recording function is evident to flight crew during preflight check e.g. by means of a system status monitor, b) Need for maintenance has been identified by system monitors, where available, with setting of an indicator and cause of that setting has not been determined, or c) Analysis of recorded data or maintenance actions have shown that more than 5% of the total number of individual parameters (variable and discrete), required to be recorded for the particular aircraft, are not being recorded properly. NOTE 2: Where improper recording affects 5% of the parameters or less, timely corrective action will need to be taken by aeroplane operator in accordance with approved maintenance procedures. be placed on FDR Control Panel and will be noted on

123 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 31-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 31. INDICATING / RECORDING SYSTEMS 3. Brake Temperature Monitoring System (BTMS) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 May be inoperative provided aeroplane is operated in accordance with AFM Appendix on Brake Kinetic Energy and Carbon Brake Cooling. NOTE: This item includes the BTMS displayed on the brakes synoptic page. 4. G Monitor System D Electronic Checklist (GV) C 2 1 May be inoperative provided the checklist module in Fault Warning Computer (FWC) 1 is operative. Electronic Checklist (GV-SP / GIV-X) C 1 0 May be inoperative provided the current AFM is carried on board the aeroplane. 6. Data Acquisition Unit (DAU) Channels (GV) B 4 3

124 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 31-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: INDICATING / RECORDING SYSTEMS 7. Security System *** MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D Engine Cowl Open *** Indicating System 9. Aeroplane Personality Modules (APM) (GV-SP, GIV-X) D 1 0 May be inoperative provided right engine cowl is visually confirmed CLOSED before starting APU on the ground. C Plastic Guard Switch Covers C - 1 May be inoperative provided APU fire bottle switch cover is installed and operative. 11. Configuration Management System (GV-SP, GIV-X) C 2 1

125 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 31-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 31. INDICATING / RECORDING SYSTEMS 12. InfraRed Counter *** Measuring System (IRCM) or Directional InfraRed Counter Measurers System (DIRCM) 13. Quick Access Recorder *** (QAR) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D 1 0 C 1 0 (M)(O) May be inoperative for Flight Data Monitoring (FDM) purposes provided approved alternate procedures, if appropriate to other programmes using associated data, are established and used. D 1 0 (M) May be inoperative provided procedures do not require its use. Maintenance will pull and collar the QAR circuit breaker. Maintenance will pull and collar the QAR circuit breaker. Flight crew will use the Event Button any time an unusual occurrence is encountered so the FDR can be downloaded for use on the flight data monitoring program. 14. XM Weather Receiver *** D 1 0

126 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 31-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 31. INDICATING / RECORDING SYSTEMS 15. Modular Avionics Unit (MAU) Channels (GV-SP/GIV-X) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 A 6 5 (M)(O) May be inoperative provided: a) Failed channel is not MAU 1A or MAU 2B, b) No other failures exist in the Avionics System, c) Associated MAU circuit breakers are pulled and collared, d) Alternate procedures are established and used, and e) Repairs are made within two (2) flight days. Maintenance will pull and collar the associated MAU circuit breakers. Flight crew will review the next worse failures as described in the GAC-OIS-09 Dispatch with MAU Channels Inoperative. Flight crew will discuss contingency procedures should the next worse failure occur and plan accordingly for the flight.

127 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 32-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: LANDING GEAR MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 1. Anti-Skid System C 1 0 (O) May be inoperative provided aeroplane is operated in accordance with AFM Limitations. 2. Rudder Pedal Steering System C 1 0 May be inoperative provided Nose Wheel Tiller Steering System is operative. Flight crew will ensure aeroplane is operated in accordance with AFM, Section 1, Limitations, Anti-Skid. (Takeoff is permitted with antiskid inoperative, provided the runway is dry, ground spoilers are operative, 20 degrees flaps are used, and the cowl and wing anti-icing system are not used.) be placed on Anti-Skid "ON/OFF" Switch and will be noted on

128 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 32-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ LANDING GEAR 3. Variable Gain Nose Wheel Steering 4. Nosewheel Steering Accessory Hardware (Torque Link Lanyards) 5. Emergency Landing Gear Extension Bottle Pressure Gauge (Nose Wheelwell) 6. Emergency Landing Gear Extension Bottle Pressure Cockpit CAS Indication (Summary Page) C 1 0 (O) May be inoperative provided the fixed gain steering mode is operative. Flight crew will verify NWS Fixed Gain is annunciated on CAS prior to dispatch. D - 0 May be inoperative or missing. B 1 0 May be inoperative provided Emergency Landing Gear Extension Bottle Pressure Cockpit CAS Indication (Summary Page) is operative and checked prior to each flight. B 1 0 May be inoperative provided Emergency Landing Gear Extension Bottle Pressure Gauge (Nose Wheelwell) is operative and checked prior to each flight.

129 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 32-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 32. LANDING GEAR 7. Landing Gear Extension / Retraction System (includes dump valve, gear handle, and blow down bottle) (GIV-X) A 1 0 (O) May be inoperative provided: a) Aeroplane is operated with the landing gear in the extended position, b) Landing gear handle remains in the down position, c) Ground lock pins are installed to ensure that all three (3) Landing gears are LOCKED down throughout flight, d) Both pilots use cockpit headsets, e) Operations are not conducted in known or forecasted icing conditions, f) Overwater flights beyond 30 minutes at normal cruising speed or 50 NM away from land, whichever is the lesser are prohibited, g) Flight is conducted in accordance with AFM Supplement No. GIV , h) Category II operations are prohibited, i) EFVS operations below 200 feet above touchdown zone elevation are prohibited, and j) Repairs are made within one (1) flight day. Flight crew will install all three landing gear ground lock pins and ensure that the pin s flags are removed prior to every takeoff.

130 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 32-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 32. LANDING GEAR 7. Landing Gear Extension / Retraction System (includes dump valve, gear handle, and blow down bottle) (GV/GV-SP) A 2 0 (O) May be inoperative provided: a) Aeroplane is operated with the landing gear in the extended position, b) Landing gear handle remains in the down position, c) Ground lock pins are installed to ensure that all three (3) Landing gears are LOCKED down throughout flight, d) Both pilots use cockpit headsets, e) Operations are not conducted in known or forecasted icing conditions, f) Overwater flights beyond 30 minutes at normal cruising speed or 50 NM away from land, whichever is the lesser are prohibited, g) Flight is conducted in accordance with AFM Supplement No. GV , h) Category II operations are prohibited, i) EFVS operations below 200 feet above touchdown zone elevation are prohibited, and j) Repairs are made within one (1) flight day. Flight crew will install all three landing gear ground lock pins and ensure that the pin s flags are removed prior to every takeoff.

131 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 33. LIGHTS 1. Cockpit/Flight Deck/ Flight Compartment Instrument Lighting Systems (Excluding EFIS and EICAS) 2. Passenger Cabin Interior Illumination Systems C - - Individual lights may be inoperative provided remaining lights are: a) Remaining Lighting System lights are sufficient to clearly illuminate all required instruments, controls and other devices for which it is provided, b) Remaining Lighting System lights are positioned so that direct rays are shielded from flight crewmembers' eyes, c) Lighting configuration and intensity is acceptable to the flight crew, and d) Emergency flight deck lighting is operative. NOTE 1: Individual button/switch lights and/or annunciations/indications are excluded from this relief. NOTE 2: Unaided operation (without NVGs) may be permitted with inoperative NVG supplemental lights; cracked or missing filters. D - - May be inoperative provided: a) Cabin emergency lighting is operative, b) Sufficient lighting is operative for crew to perform required duties, and c) Lighting configuration at dispatch is acceptable to flight crew. be placed above the affected Lighting Rheostat and will be noted on be placed on affected Cabin Interior "ON/OFF" Switch and will be noted on

132 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ LIGHTS 3. Passenger Lighted Information Signs 1) All Cargo Supernumerary/ Courier Area Lighted Information Signs (continued) C - - (M) May be inoperative provided: a) Associated passenger seat or lavatory is not occupied from which a passenger lighted information sign is not readily legible, and b) Associated seat or lavatory is blocked and placarded - DO NOT OCCUPY. NOTE: These conditions are not intended to prohibit lavatory use or inspections by crewmembers. C - - (O) May be inoperative and associated passenger seat or lavatory may be occupied provided alternate procedures are established and used to notify passengers and cabin crew when associated sign(s) is placed ON or OFF. C - - (O) May be inoperative provided alternate procedures are established and used to notify couriers/supernumeraries when associated sign(s) are placed ON or OFF. Maintenance will ensure: a) Associated passenger seat or lavatory is not occupied, and b) Associated seat or lavatory is blocked and placarded DO NOT OCCUPY. Flight crew will notify the passengers and cabin crew by a series of chimes from the passenger notification system or by person to person contact. Flight crew will notify the passengers and cabin crew by a series of chimes from the passenger notification system or by person to person contact. be placed on associated seat or lavatory stating DO NOT OCCUPY and will be noted on be placed on inoperative PA System and will be noted on be placed in a prominent position to notify courier/ supernumerary when associated sign(s) are placed ON or OFF and will be noted on

133 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ LIGHTS 3. Passenger Lighted Information Signs (cont d) The following pertains only to operations involving aircraft with 19 or less passenger seats, wherein certificatin or operating rules do not require a public address system or flight attendant. 2) Passenger Lighted Information Signs C - - (O) May be inoperative provided alternate procedures are established and used to notify cabin occupants. Flight crew will ensure alternate procedures are established and used. An Inoperative placard will be placed on inoperative Passenger Lighted Information Signs and will be noted on 4. Position Light Bulbs C 6 3 May be inoperative provided one light bulb is operative at each position. C 6 0 May be inoperative provided aeroplane is not operated at night. be placed on Position (Navigation) Light "ON/OFF" Switch and will be noted on be placed on Position (Navigation) Light "ON/OFF" Switch and will be noted on

134 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: LIGHTS MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 5. Beacon Light C 1 0 May be inoperative provided aeroplane is not operated at night. 6. Strobes (Anti-Collision Lights) 7. Wing Inspection Lights (Aeroplanes with wing critical surfaces not visible from flight deck) C 1 0 May be inoperative provided Strobes are installed and operative. C 6 3 Bulbs may be inoperative provided one bulb is operative at each position (wingtip and tail). C 6 2 May be inoperative provided: a) At least one bulb is operative at each wingtip, and b) Aeroplane is not operated at night. C 2 0 May be inoperative provided ground deicing procedures do not require their use. be placed on Beacon Light "ON/OFF" Switch and will be noted on be placed on Beacon Light "ON/OFF" Switch and will be noted on be placed on Strobe "ON/OFF" Switch and will be noted on be placed on Strobe "ON/OFF" Switch and will be noted on be placed on Wing Inspection Light "ON/ OFF" Switch and will be noted on

135 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: LIGHTS MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 8. Landing Lights B 2 1 May be inoperative provided all three bulbs of the taxi lights are operative. be placed on affected Landing Light (L LDG) or (R LDG) "ON/OFF" Switch(es) and will be noted on C 2 0 May be inoperative provided aeroplane is not operated at night. be placed on affected Landing Light (L LDG) or (R LDG) "ON/OFF" Switch(es) and will be noted on 9. Taxi Light System C 1 0 be placed on Taxi "ON/OFF" Switch and will be noted on 1) Individual Light Bulbs 10. Wing Tip Taxi *** Light Systems C 3 0 be placed on Taxi "ON/OFF" Switch to indicate the inoperative light bulbs and will be noted on D 2 0 be placed on Wing Tip Taxi "ON/OFF" Switch and will be noted on

136 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ LIGHTS 11. Floor Proximity *** Emergency Escape Path Marking System Lights a) Individual Lights / Strips 12. Pulse Light System *** (Identification Lights) 13. Recognition Light *** System 14. Logo Light *** System B - - Lights / strips may be inoperative provided: a) All lights/strips marking right angle intersection, including overwing exits, are operative, b) Along each aisle axis, all lights/strips within one meter of lights/strips marking right angle intersections are operative, and c) Along each aisle axis, for a particular lights/strips configuration, specific lights/strips are operative as agreed by the Authority. D - 0 be displayed on affected Pulselight System Light Switch and will be noted on D 1 0 be displayed on affected Recognition Light Switch and will be noted on D 1 0 be displayed on affected Logo Light Switch and will be noted on

137 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ LIGHTS 15. Ramp Lights *** Systems 16. Torch Charging *** Systems 17. Aft Compartment Lights (Boiler Room) 18. Cargo Compartment *** Light 19. Pylon Mounted *** Exterior Baggage Loading Light Systems D - 0 be displayed on affected Ramp Light Switch and will be noted on D - 0 D - 0 be placed nest to Aft Compartment Light Switch and will be noted on D 1 0 May be inoperative provided no emergency equipment is carried in the Cargo Compartment. D 1 0 May be inoperative provided an operative torch is installed in Cargo Compartment. D - 0

138 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-8 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 33. LIGHTS MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ Wheel Well Lights D Exterior Emergency Evacuation Lighting System B 1 0 May be inoperative provided aeroplane is operated during daylight only. 22. Service Door Lights D Dim and Test Enunciator Channels C - - May be inoperative provided the switch capsule is not used in an emergency procedure where the actuation of the switch is not displayed elsewhere in the cockpit. NOTE: The following switches 1-4 may not be inoperative: 1. GPWS / Ground Spoiler Override 2. Terrain Display (GV) / Terrain Inhibit (GV-SP) 3. CPCS Panel Flight / Landing (2) 4. Door Safety

139 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 33-9 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 33. LIGHTS MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ Airstair Lights D - 0 May be inoperative provided an alternate means (e.g. torch) is used to illuminate the airstairs. 25. Dome Light D - 0 May be inoperative provided an alternate means (e.g. torch) is used to illuminate the vestibule area. 26. Baggage Compartment Light D 1 0 May be inoperative provided no emergency equipment is carried in the baggage compartment. D 1 0 May be inoperative provided an operative torch is installed in the baggage compartment. 27. Torches C - 2 One or more may be inoperative provided each required crewmember assigned to affected positon has an operative torch.

140 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ LIGHTS 28. Wing Tip Position *** Light LED Element Banks C 4 2 One may be inoperative per wing tip position. C 4 0 May be inoperative provided aeroplane is not operated at night. 29. Tail Position Light *** LED Element Banks C 2 1 C 2 0 May be inoperative provided aeroplane is not operated at night.

141 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 1. Directional Compass Reference Sensors B 3 2 (O) May be inoperative provided both PFD Heading Indicating Systems operate independently. Flight crew will ensure that the same IRS is NOT used as the heading source for both pilots. be placed on Mode Select Unit (MSU) and will be noted on 2. Attitude Reference Sensors B 3 2 (O) May be inoperative provided: a) Both PFD Attitude Indicating Systems operate independently, and b) Standby Attitude Indicator is operative. Flight crew will ensure same IRS is NOT used as attitude source for both pilots. be placed on MSU and will be noted on 3. Standby Flight Displays 1) Standby Attitude *** Indicator (Electro- Mechanical Gyro Horizon) *** a) Glideslope/ Localizer Indicator (continued) C - 0 Except for ER operations, may be inoperative provided it is not required by Operating Requirements. B - 0 May be inoperative provided Operations are conducted in day VMC only C 1 0 May be inoperative provided aeroplane is operated in day VMC only. be placed on face of Standby Attitude Indicator and will be noted on

142 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 3. Standby Flight Displays (cont d) *** 2) Standby Altimeter/ Airspeed Indicator (combined unit) *** 3) 3-in-1 Standby Attitude, Altitude, Airspeed Indicator Heading (Color Video Display) (GV Only) *** a) Standby Air Data Unit(Altitude and Airspeed Function) *** b) Standby Heading Display (continued) C 1 0 May be inoperative provided aeroplane is operated in day VMC only. C - 0 Except for ER operations, the Attitude position indicator may be inoperative provided not required by Operating Requirements. B - 0 Attitude position indicator may be inoperative provided: a) Operations are conducted in Day VMC only, and b) Operations are not conducted into known or forecast VFR-on-Top Conditions. C 1 0 May be inoperative provided the aeroplane is operatedin day VMC only. C 1 0 May be inoperative provided all three (3) Heading Reference Systems are operative. None requird.

143 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 34. NAVIGATION 3. Standby Flight Displays (cont d) *** 3) 3-in-1 (Color Video Display) (GV Only) (cont d) *** c) Glideslope / Localizer Function MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 *** d) DME Displays C - 0 *** e) FMS Navigation Functions (continued) C 1 0

144 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 3. Standby Flight Displays (cont d) *** 4) 4-in-1 Standby Attitude, Altitude, Airspeed Indicator Heading (Color Video Display) (GV-SP, GIV-X) *** a) Standby Air Data Unit (Altitude and Airspeed Function) *** b) Standby Heading Display (continued) C - 0 Except for ER operations, the Attitude position indicator may be inoperative provided not required by Operating Requirements. B - 0 Attitude Position indicator may be inoperative provided: a) Operations are conducted in Day VMC only, and b) Operations are not conducted into known or forecast VFR-on-Top Conditions. C 1 0 May be inoperative provided the aeroplane is operated in day VMC only. C 1 0 May be inoperative provided all three (3) Heading Reference Systems are operative.

145 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 34. NAVIGATION 3. Standby Flight Displays (cont d) *** 4) 4-in-1 (Color Video Display) (GV-SP, GIV-X) (cont d) *** c) Glideslope/ Localizer Function MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 *** d) DME Displays C - 0 *** e) FMS Navigation Functions 4. Weather Radar Systems C 1 0 C - - Except for ER operations, one or more system(s) may be inoperative provided the weather reports or forecasts available to the commander indicate that cumulinimbus clouds or other potentially hazardous weather conditions, which could be detected by the system(s) when in working order, are unlikely to be encountered on the intended route of any planned diversion therefrom. be placed on Radar Control Heads and will be noted on

146 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 5. VOR/ILS Navigation Systems 6. Marker Beacon Systems 7. Automatic Direction Finding (ADF) Systems C - - As required by Operating Requirements and no relief may be provided to an inoperative system or component if powered by an emergency bus. B - 0 One or more may be inoperative for IFR operations, provided approach procedures do not require marker fixes. D - 0 One ore more may be inoperative for VFR operations. C 2 0 (O) One or both may be inoperative provided: a) The navigation systems required for each segment of the intended route are operative, and b) Alternate procedures are established and used where applicable. NOTE: The intended route corresponds to any point on the route including diversions to reach alternate aerodromes required to be selected by the operational rules be placed on affected RFMU and will be noted on Flight crew shall give alternate procedure sin case existing operational procedures are affected. be placed on or next to affected ADF Indicator and will be noted on

147 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 34. NAVIGATION 8. SSR Transponder 1) Mode A/C Functions MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C - - Any in excess of those required for the route to be flown may be inoperative. A - 0 (O) May be inoperative for a maximum of 5 flights provided: a) Permission is obtained from the Air Navigation Service Provider(s) along the route of any planned diversions, and b) Flight is conducted under VFR over routes navigated by reference to visual landmarks. NOTE: Mode C function is required to operate for RVSM operations. 2) Mode S Function D - 0 Any in excess of those required for the route to be flown may be inoperative. (continued) NOTE: A SSR transponder with an operative MODE S function is defined as a transponder which can provide at least elementary Surveillance capability. C - 0 One or more may be inoperative provided permission is obtained from the Air Navigation Service Provider(s) when required for the intended route. NOTE 1: A SSR transponder with an operative MODE S function is defined as a transponder which can provide at least elementary Surveillance capability. Flight crew will coordinate with the appropriate ANSP for permission to fly with inoperative Mode A or C. Flight crew will conduct the flight under VFR conditions over routes navigated by reference to visual landmarks to prevent getting lost.

148 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-8 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 8. SSR Transponder 2) Mode S Function (cont d) 3) Enhanced Surveillance Functions (if installed) 9. Distance Measuring Equipment (DME) Systems NOTE 2: Altitude reporting, provided by an SSR transponder Mode S function, is required for ACAS II operation. Refer to item for flight with ACAS II inoperative. NOTE 3: Altitude reporting, provided by an SSR transponder Mode S function, is required for flight into RVSM airspace. D - 0 One or more Downlink Aircraft Parameters (DAP s), which provided Enahnced Surveillance, may be inoperative when not required for the intended route. C - 0 One or more Downlink Aircraft Parameters (DAP s), which provided Enahnced Surveillance, may be inoperative when required for the intended route. D - - Except when en route operations or approach minimums require its use, any in excess of those required by Operating Requirements may be inoperative.

149 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 34-9 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: NAVIGATION 10. Standby RMI *** (Electro-Mechanical) (GV) *** 1) Standby Navigation Display (Color Video) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: C 1 0 May be inoperative provided all three (3) IRS's are operative. C 1 0 May be inoperative provided all three (3) IRS s are operative. be placed on Standby RMI (GV) and will be noted on be placed on the Standby Navigation Display and will be noted on *** 2) DME Displays C 2 0 *** 3) EBDI (Electronic Bearing / Distance Indicator (GV-SP/GIV-X) 11. Radio Altimeter Systems C 1 0 May be inoperative provided all three (3) IRS s are operative. C 2 0 May be inoperative provided: a) Landing weather minimums or operating procedures do not require its use, and b) Other systems affected (E/GPWS, ACAS, Flight Director, Autopilot, Autothrottle, Altimeter Ground Awareness Display, Synthetic Vision Primary Flight Dispaly) are considered. be placed on the EBDI and will be noted on

150 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 12. Long Range Navigation Systems (IRS, GPS and GNSSU) 13. Ground Proximity Warning System 1) Glideslope Deviation (Mode 5) (continued) C - - May be inoperative except where en route operations or approach minimums require the use of GPS or GNSSU. NOTE: For flights conducted in RNP4 airspace, both GPS receiver must be operative. C - - As required by Operating Requirements. NOTE: IRS Navigation Function only. See Attitude Reference Sensors for IRS Attitude Function. A - 0 May be inoperative provided repairs or replacements are carried out within 6 further flight or 25 flying hours or 2 calendar days, whichever occurs first. NOTE: If any of the Terrain Avoidance Modes 1-4 or the Test Mode is inoperative, then the GPWS is considered inoperative. be placed on affected Instrument Controller and will be noted on be placed on affected Instrument Controller and will be noted on B - 0 May be inoperative. C - 0 May be inoperative for day VMC only.

151 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 13. Ground Proximity Warning System (cont d) 2) Advisory Callouts *** C - 0 (O) May be inoperative provided alternate procedures are established and used. NOTE: Check Flight Manual limitations for approach minimums. Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations. 3) Windshear Mode *** C - 0 (O) May be inoperative provided alternate procedures are established and used. Flight crew will comply with AFM/AOM guidance in windshear situations and recommend procedures when encountering windshear. 4) Terrain Awareness & Warning System (TAWS) (where required) A - 0 May be inoperative provided: a) GPWS function are operative, and b) Repairs or replacements are carried out within 10 calendar days. 5) Runway *** Awareness and Advisory System (RAAS) C 1 0 6) Windshear *** Mode (Reactive) (continued) D - 0 (O) May be inoperative provided: a) At least one (1) radio altimeter is available, and b) Alternate procedures are established and used. Flight crew will comply with AFM/AOM guidance in windshear situations and recommend procedures when encountering windshear.

152 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 13. Ground Proximity Warning System (cont d) 7) Terrain Display *** 14. Lasertrak NDU *** (GV) C - 1 B - 0 C 1 0 May be inoperative provided at least one Flight Management System is operative.

153 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 15. Flight Management Systems (CDU and Nav Computer Only) (GV only) 1) Navigation Database(s) NOTE: Database(s) which is/are out of date is/are considered to be inoperative B - 0 Except where en route operations or approach minimums require its use, may be inoperative provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, and d) Both RFMUs are operative. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. C - 0 (O) One or more may be inoperative for the intended route where conventional (non-rnav) navigation is sufficient provided: a) Current aeronautical information (e.g. Charts) is available for the entire route and for the aerodromes to be used, and b) Navigation databases information is disregarded. be placed adjacent to the CDU and will be noted on Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will disregard navigation data base information. (continued)

154 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 15. Flight Management Systems (CDU and Nav Computer Only) (GV only)(cont d) 1) Navigation Database(s) (cont d) (continued) C - 1 Any in excess of one may be inoperative provided: a) Operative database must be up to date for routes, departures, arrival and approach procedures that require use of navigation Database for RNAV, and b) This up to date Database is readily available to flight crewmember(s) responsible for navigation. A - 0 (O) One or more may be out of date for maximum of 10 calendar days provided: a) Aero Navigation (RNAV) departure, arrival and approach procedures do not depend on data amended in current database cycle, b) Before each flight, current aeronautical information is used to verify database Navigation Fixes, the coordinates, frequencies status (as applicable) and suitability of Navigation Facilities required for intended route, and c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, and which have been amended in current database cycle are manually tuned and identified. be placed adjacent to the CDU and will be noted on Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will verify navigation database information using current aeronautical information before each flight. Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

155 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 15. Flight Management Systems (CDU and Nav Computer Only) (GV only)(cont d) 1) Navigation Database(s) (cont d) A - 0 (O) One or more may be out of date for maximum of 10 calendar days provided: a) Conventional (Non-RNAV) departure, arrival and approach procedures, when available, or ANSP assistance are used as an alternative to RNAV procedures which have been amended in the current database cycle, b) Before each flight, current aeronautical information is used to verify database Navigation Fixes. The coordinates, frequencies, status (as applicable) and suitability of Navigation Facilities required for intended route, and c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, and which have been amended in current database cycle are manually tuned and identified. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will verify navigation database information using current aeronautical information before each flight. Flight Crew will manually tune and identify all radio navigation aids used throughout the flight. be placed adjacent to the CDU and will be noted on

156 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 16. Navigation Management Systems B - 0 Except where en route operations or approach minimums require its use, may be inoperative provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not depend on its use, and d) Both RFMUs must be operative. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) sytem is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. 1) Navigation Database(s) Note: Database(s) which is/are out of date is/are considered to be inoperative (continued) C - 0 (O) One ore more may be inoperative for the intended route where conventional (non-rnav) navigation is sufficient provided: a) Current aeronautical information (e.g. Charts) is available for the entire route and for the aerodromes to be used, and b) Navigation Databases information is disregarded. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will disregard navigation data base information

157 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 16. Navigation Management Systems 1) Navigation Database(s) (cont d) (continued) C - 1 Any in excess of one may be inoperative provided: a) Operative database must be up to date for routes, departures, arrival and approach procedures that require use of navigation Database for RNAV, and b) This up to date Database is readily available to flight crewmember(s) responsible for navigation. A - 0 (O) One or more may be out of date for maximum of 10 calendar days provided: a) Aero Navigation (RNAV) departure, arrival and approach procedures do not depend on data amended in current database cycle, b) Before each flight, current aeronautical information is used to verify database Navigation Fixes, the coordinates, frequencies, status (as applicable) and suitability of Navigation Facilities required for intended route, and c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, and which have been amended in current database cycle are manually tuned and identified. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will verify navigation database information using current aeronautical information before each flight. Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

158 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 16. Navigation Management Systems 1) Navigation Database(s) (cont d) A - 0 (O) One or more may be out of date for maximum of 10 calendar days provided: a) Conventional (Non-RNAV) departure, arrival and approach procedures, when available, or ANSP assistance are used as an alternative to RNAV procedures which have been amended in current database cycle, b) Before each flight, current aeronautical information is used to verify database Navigation Fixes. The coordinates, frequencies, status (as applicable) and suitability of Navigation Facilities required for intended route, and c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, and which have been amended in current database cycle are manually tuned and identified. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will verify navigation database information using current aeronautical information before each flight. Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

159 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 34. NAVIGATION 17. Lightning Sensor *** Systems (LSS) 18. Stormscope *** 19. Airborne Collision Avoidance System (ACAS) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D - 0 D - 0 1) ACAS System A - 0 (M)(O) May be inoperative for a maximum of 10 calendar days provided the system is deactivated and secured. 2) Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System(s) (continued) C 2 1 (O) May be inoperative on the non-flying pilot side provided: a) TA and RA visual display is operative on the flying pilot side, and b) TA and RA audio function is operative on the flying pilot side. Maintenance or qualified flight crew will ensure system is deactivated by pulling and collaring ACAS Power circuit breaker. Flight crew will follow flight plan to avoid airspace where an operating ACAS is required, e.g., RVSM airspace. Flight crew will ensure the pilot flying has the operative TA and RA visual displays. Flight crew will perform an ACAS system test prior to first flight of the day.

160 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 19. Airborne Collision Avoidance System (ACAS)(cont d) 3) Resolution Advisory (RA) Display System(s) 4) Traffic Alert (TA) Display System(s) 5) Airspace Selection *** Function (Above / Normal / Below) C 2 1 (O) May be inoperative on non-flying pilot side. C - 0 (O) One may be inoperative provided: a) All Traffic Alert (TA) display elements and voice command audio functions are operative, and b) TA only mode is selected by the crew. C - 0 (O) One or more may be inoperative provided all installed RA display and audio functions are operative. Flight crew will ensure that the pilot-flying has an operative RA display system. Flight crew will test the ACAS to ensure that the TA display and aurals are operative prior to first flight of the day. Flight crew will select TA only mode for the ACAS. Flight crew will test the ACAS to ensure that the RA display and aurals are operative prior to first flight of the day. C - 0

161 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 20. Microwave Landing *** Systems (MLS) C - 0 May be inoperative provided approaches and missed approaches where navigation is based on MLS are not included in the flight plan. 21. Symbol Generators (GV) C 3 2 (M)(O) May be inoperative provided: a) EFIS displays at pilot s and copilot's stations are operative from independent Symbol Generators, and b) Both EICAS displays are operative. Maintenance should move inoperative SG to No. 3 position. Refer to AMM chapter Maintenance will pull and collar the SG 3 circuit breaker. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will ensure EFIS Displays at pilot's and copilot's stations are operative from Independent Symbol Generators, and BOTH EICAS Displays (DU 3 and 4) are operative. Crew WILL select ALT for No. 3 SG to power EICAS displays. 22. Guidance Panel Digital Indications and Mode Select Indications 1) Speed Display C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. (continued)

162 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 34. NAVIGATION 22. Guidance Panel Digital Indications and Mode Select Indications (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 2) Heading Display C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 3) VS/FPA Display C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 4) Altitude Select Display C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 5) LNAV C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 6) VNAV C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. (continued)

163 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 34. NAVIGATION 22. Guidance Panel Digital Indications and Mode Select Indications (cont d) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 7) FLCH C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 8) Manual Speed C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 9) Bank Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 10) BC Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 11) Heading Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. (continued)

164 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: NAVIGATION MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 22. Guidance Panel Digital Indications and Mode Select Indications (cont d) 12) VS/FPA Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 13) Alt Hold Select C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 14) Approach C 1 0 May be inoperative provided the associated value is available in the Primary Flight Display. 15) PFD Command L/R C 1 0 (O) May be inoperative provided the associated value is available in the Primary Flight Display. On initial power up of the aeroplane, the default is PFD command left PFD. If button is pushed several times, PFD command to the left PFD can be established by pulling and resetting Guidance Panel circuit breakers. 16) APR Switch C 1 0 May be inoperative provided the associated status is available in the Primary Flight Display.

165 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 23. Altitude Alerting System 24. Display Units (GV) (continued) B - 0 (O) May be inoperative provided an autopilot with an altitude hold is operative. NOTE: One altitude alerting system is required to be operative for RVSM operations. C 6 5 (M)(O) May be in operative provided: a) The inoperative unit is located in the Copilot's Navigation Display Position (DU #5), b) Standby Attitude Indicator is operative, c) Standby RMI is operative, and d) Alternate procedures are developed for operation without the Copilot's Navigation displays. Maintenance will move the inoperative display unit to the Copilot's Navigation Display Position (DU #5). Refer to AMM chapter Maintenance will pull and collar the DU#5 circuit breaker. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will ensure Autopilot with Altitude Hold is operable. NOTE: Flight into RVSM airspace is not allowed with inoperative Altitude Alerting System. Flight crew will ensure Standby Attitude Indicator and Standby RMI are operative. Alternate Procedures for operation without Copilot's Navigation Display (Pre-Takeoff and Pre- Arrival Crew Briefings) should include crew actions in the event of failure of another DU. Factors concerning abort criteria, takeoff continuance, deviation to alternate airfield and mission continuance should be included in there briefings. For an approach with both copilot's PFD and ND inoperative, it is recommended that Compass Mode be selected on pilot's ND.

166 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 24. Display Units (cont d) *** Display Units (GV) For DU-885 Equipped Aeroplanes (continued) C 6 5 (M)(O) May be inoperative provided: a) The inoperative unit is located in the Copilot s Navigation Display Position (DU #5), b) Standby Attitude Indicator is operative, c) Standby RMI is operative, d) Alternate procedures are developed for operation without the Copilot s Navigation displays, and e) Terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Maintenance will move the inoperative display unit to the Copilot's Navigation Display Position (DU #5). Refer to AMM chapter Manintenance will pull and collar DU#5 curcuit breaker. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will ensure the following: a) Standby Attitude Indicator and Standby RMI are operative, b) Alternate Procedures for operation without Copilot's Navigation Display (Pre- Takeoff and Pre-Arrival Crew Briefings) should include crew actions in the event of failure of another DU, c) Factors concerning abort criteria, takeoff continuance, deviation to alternate airfield and mission continuance should be included in their briefings, and d) Terminal charts for origin, destination and alternate airports are verified to be current and onboard the aircraft. For an approach with both copilot's PFD and ND inoperative, it is recommended that Compass Mode be selected on pilot's ND.

167 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 24. Display Units (cont d) Display Units (GV-SP, GIV-X) 25. Standby Magnetic Compass System (Flux Valve) (GV) C 4 3 (M)(O) May be inoperative provided: a) The inoperative unit is located in the DU #3 position, and b) The pilot in the left seat flies the aeroplane. C 1 0 May be inoperative provided all three (3) Heading Reference systems are operative. Maintenance will move the inoperative display unit to the DU3 position. Refer to AMM Chapter Maimtenance will pull and collar DU#3 circuit breaker. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will discuss alternate procedures for loss of a second display for all phases of flight including failures during takeoff, approach, landing, and go-around. It is required that the pilot in the left seat fly the aeroplane. *** Magnetometer (GV-SP, GIV-X) C 1 0 May be inoperative provided all three (3) IRS s are operative.

168 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 26. Non-Stabilized *** Magnetic Compass B 1 0 May be inoperative provided any combination of three (3) Gyro or INS (IRU) Stabilized Compass Systems are operative. B 1 0 May be inoperative provided: a) Any combination of two(2) Gyro or INS (IRU) Stabilized Compass Systems are operative, and b) Aeroplane is operated with Dual Independent Navigation Capability and under Positive Radar Control by ATC on the en route portion of the flight. B 1 0 May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are installed, operative, and used in conjunction with accepted Free Gyro Navigation Techniques.

169 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 27. Head Up Display *** System 28. Airborne Flight *** Information System (AFIS) D 1 0 May be inoperative provided landing weather minimums or operating procedures do not require its use. D - 0 NOTE: The relief includes the datalink function (GV, GV-SP, GIV-X) and ADS- A/ADS-C function (GV-SP, GIV-X) 1) AFIS Printer D - 0 be placed on AFIS Printer and will be noted on 29. Slip-Skid Indicator B 2 1 May be inoperative provided: a) Third attitude indicator is installed and operative, and b) An operative slip indication is obtained by selecting another IRS source via the Display Controller. (GV Only) B 2 1 (O) May be inoperative provided electronic slip indicator is replaced by a mechanical slip indicator. B 2 0 May be inoperative provided aeroplane is operated during day VMC conditions. Flight crew will ensure mechanical slip indicator is installed.

170 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 30. Data Loader *** (GV) Data Management Unit (DMU) (GV-SP, GIV-X) 31. Air Data Computers/ Systems 1) Micro Air Data Computers (GV) (continued) D 1 0 D - 0 C 3 2 (M) (O) May be inoperative provided: a) Manual Pressurisation Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, and e) Aeroplane is operated in accordance with AFM Limitations. NOTE: Two systems are required for operation in RVSM airspace. Maintenance will pull and collar circuit breaker associated with inoperative Micro Air Data Computer. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will operationally check and assure that the items called out in provisos a) thru d) are operative. Flight crew will comply with all AFM limitations in Section , , and be placed on Micro Air Data Computers to be seen by flight crew and will be noted on

171 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 31. Air Data Computers/ Systems (cont d) 1) Micro Air Data Computers (GV) (cont d) (continued) C 3 2 May be inoperative provided aeroplane is operated in unpressurised configuration. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed on Micro Air Data Computers to be seen by flight crew and will be noted on

172 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 31. Air Data Computers/ Systems (cont d) 2) Air Data Systems (ADS) (GV-SP, GIV-X) 32. Integrated Avionics *** Computers (IACs) (GV) C 3 2 (M) May be inoperative provided: a) Manual Pressurisation Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, and e) Aeroplane is operated in accordance with AFM Limitations. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: If ADS 2 is failed, the WOW indications on the copilot s flight control synoptic will be crosshatched. Dispatch is still allowed if the WOW indications on the pilot s flight control synoptic are shown as valid. C - 2 May be inoperative provided two bus controllers are operative for dispatch. NOTE: The FMS/PMS/Autothrottle function of the operative IACs may be inoperative as stated elsewhere in this section. The autopilot is addressed in ATA 22. Maintenance will pull and collar the ADM circuit breaker associated with the inoperative ADS. Flight crew may accomplish this task if properly qualified and authorised. be placed on Air Data Systems to be seen by flight be will be placed on Integrated Avionics Computers (IACs) to be seen by flight crew and will be noted on

173 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 33. Bus Controllers (GV) 34. Airshow Controller *** System 1) Cockpit Airshow *** Display System 2) Cabin Airshow *** Display System C - 2 D - 0 D - 0 D - 0

174 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 35. Windshear Warning *** and Flight Guidance System (Reactive) 36. Windshear Detection *** and Avoidance System (Predictive) 37. Cockpit Video *** Monitors 38. Heads Up Checklist *** C - 0 (O) May be inoperative provided alternate procedures are established and used. C - 0 (O) May be inoperative provided alternate procedures are established and used. Flight crew will comply with the AFM/AOM guidance on windshear conditions and the recommended procedures for windshear encounters. Flight crew will comply with the AFM/AOM guidance on windshear conditions and the recommended procedures for windshear encounters. D - 0 D - 0

175 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 34. NAVIGATION 39. Enhanced Vision *** System (EVS) 1) EVS Window *** Heat 2) Secondary (non- *** HUD) EVS Display Repeater MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D 1 0 D 1 0 D 1 0 May be inoperative provided procedures are not dependent on its use. 40. Terrain Server C Function/EGPWM 2 0 May be inoperative provided: Function/EGPWM a) GPWS functions are operative, and Modules (GV-SP, GIV-X) b) Repairs or replacements are carried out within 10 Calendar days. NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction.

176 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 41. Advanced Graphics Modules (AGM) (GV-SP, GIV-X) Advanced Graphics Module (AGM) (GV-SP, GIV-X) (ASC Cert Charlie and ASC 905 Cert Charlie II and Any later revision to the Operating software) C 4 3 (M)(O) May be inoperative provided: a) The inoperative AGM is located in the AGM 3 position, and b) Crew actions for subsequent failures are established. C 4 3 (O) May be inoperative provided: a) The inoperative AGM is electronically switched to the AGM 3 position resulting in DU3 Red Xing, and b) Crew actions for subsequent failures are established. Maintenance will move the inoperative AGM module to the AGM 3 position. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will discuss the alternate procedures for sharing displays including if a display fails during all phases of flight including takeoff, approach, landing, and go-around. Flight crew will ensure: a) The failed AGM is electronically switched to the number 3 position, b) Verify that DU 3 is Red X ed prior to dispatch, c) Dim DU 3 to eliminate the Red X, and d) Discuss alternate procedures for sharing displays in the event a second AGM or DU fails during any phase of flight NOTE: Refer to AFM Sections /261 and Section Cockpit Printer D 1 0

177 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 43. Cursor Control Devices (GV-SP, GIV-X) *** Cursor Control Devices (GV Only) C 2 0 May be inoperative provided a) Both Display Controllers, Weather Radar Controllers, and 2 MCDU s are operative, and b) Terminal charts for the origin, destination and alternate airports are verified to be current and onbard the aircraft. C 2 0 (M)(O) May be inoperative provided: a) Both Display Controllers are operative, and b) Terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Maintenance will pull and collar the circuit breaker for the inoperative CCD. Flight crew will ensure that terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft.

178 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 44. Multifunction Control Display Units (MCDU) (GV-SP, GIV-X) 1) Flight Management System (FMS) Functions (GV-SP, GIV-X) (continued) C 3 2 (M) May be inoperative provided: a) The FMS functions and Radio Tuning functions are operative on the remaining MCDU s, and b) The inoperative MCDU is located in either the No. 1 or the No. 2 position. NOTE: MCDU 1 has Standby Engine instruments. MCDU 3 has Backup Radio Tuning functions. B 3 1 Except where en route operations or approach minimums require its use, may be inoperative provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, and c) Procedures do not require its use. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. RNP RNAV including PRNAV and BRNAV only require a single FMS. Maintenance will perform procedures in accordance with AMM Chapter The inoperative MCDU will be moved to either the No. 1 or the No. 2 position. Maintenance will pull and collar the circuit breaker for MCDU 2.

179 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 44. Multifunction Control Display Units (MCDU) (GV-SP, GIV-X) (cont d) a) Navigation Database(s) Note: Database(s) which is/are out of date is/are considered to be inoperative C - - (O) One or more may be inoperative for the intended route where conventional (non-rnav) navigation is sufficient provided: a) Current aeronautical information (e.g. Charts) is available for the entire route and for the aerodromes to be used, and b) Navigation databases information is disregarded. C - 1 Any in excess of one may be inoperative provided: a) Operative database must be up to date for routes, departures, arrival and approach procedures that require use of navigation Database for RNAV, and b) This up to date Database is readily available to flight crewmember(s) responsible for navigation. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will disregard navigation database information.

180 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 44. Multifunction Control Display Units (MCDU) (GV-SP, GIV-X) (cont d) a) Navigation Database(s) Note: Database(s) which is/are out of date is/are considered to be inoperative (continued) A - 0 (O) One or more may be out of date for maximum of 10 calendar days provided: a) Aero Navigation (RNAV) departure, arrival and approach procedures do not depend on data amended in current database cycle, b) Before each flight, current aeronautical information is used to verify database Navigation Fixes, the coordinates, frequencies, status (as applicable) and suitability of Navigation Facilites required for intended route, and c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, which have been amended in current database cycle are manually tuned and identified. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will verify navigation database information using current aeronautical information before each flight. Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

181 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 44. Multifunction Control Display Units (MCDU) (GV-SP, GIV-X) (cont d) a) Navigation Database(s) Note: Database(s) which is/are out of date is/are considered to be inoperative 2) Radio Tuning Functions (GV- SP, GIV-X) A - 0 (O) One or more may be out of date for maximum of 10 calendar days provided: a) Conventional (Non-RNAV) departure, arrival and approach procedure, when available, or ANSP assistance are used as an alternative to RNAV procedures which have been amended in the current database cycle, b) Before each flight, current aeronautical information is used to verify database Navigation Fixes. The coordinates, frequencies, status (as applicable) and suitability of Navigation Facilites required for intended route, and c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, which have been amended in current database cycle are manually tuned and identified. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will verify navigation database information using current aeronautical information before each flight. Flight Crew will manually tune and identify all radio navigation aids used throughout the flight. B 3 2

182 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: NAVIGATION 45. Advanced Graphics Module (AGM) Databases (GV-SP, GIV-X) Note: Database(s) which is/are out of date is/are considered to be inoperative 46. Charts Function (GV-SP, GIV-X, GV for DU-885 Equipped Aeroplanes) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: A - 0 (O) One or more may be out out of date for maximum of 10 calendar days provided: a) Before each flight, current aeronautical information is used to verify database Navigation Fixes. The coordinates, frequencies, status (as applicable) and suitability of Navigation Facilities required for intended route, and b) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, and which have been amended in current database cycle are manually tuned and identified. D 2 0 May be inoperative provided current aeronautical charts are carried onboard the aeroplane and available to the flight crew. 1) Charts Database C 4 0 May be out of currency provided the terminal charts for the origin, destination, and alternate airports are verified to be current. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will verify navigation database information using current aeronautical information before each flight. Flight Crew will manually tune and identify all radio navigation aids used throughout the flight.

183 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 47. Video Function (GV-SP, GIV-X) D 1 0 May be inoperative provided alternate procedures are established for the use of the Enhanced Vision System (EVS) display function. 48. Automatic Dependent *** Surveillance-Broadcast (ADS-B) System Extended Squitter (ADS-B Out) Transmissions D - 0 One or more extended squitter transmissions may be inoperative when not required for the intended route.

184 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 49. Right Side Display Controller (GV Only) A 1 0 (M) (O) May be inoperative provided: a) The weather at the destination is forecast to be VFR (1,000 ft ceiling and three (3) miles visibility), b) Weather forecast at the alternate airport meet the same requirements as specified for the destination (1,000 ft ceiling and three (3) miles visibility), c) Both VOR and ADF navigation receivers are operative, d) Flight is conducted based on short range navigation sources only being available, e) Navigation suffix in the IFR flight plan clearly indicates that the aeroplane is not capable of any RNP required navigation capability, f) Flight is conducted in airspace where the availability of navigation by short range navigation receivers (VOR/ADF) is assured, g) One DBDI or Standby RMI or Secondary Navigation Display is operative, h) Associated Display Controller circuit breaker is pulled and collared, i) Alternate procedures are established and used, and j) Repairs are made within one (1) flight day. Maintenance will ensure associated Display Controller circuit breaker for the failed Display Controller is pulled and collared. The flight crew shall prepare and display a TOLD (Takeoff and Landing Data) card pror to takeoff and prior to approach and landing. be placed on the Right Side Display Controller and will be noted on

185 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NAVIGATION 49. Right Side Display Controller (GV-SP/GIV-X Only) A 1 0 (M)(O) May be inoperative provided: a) FMS is the navigation source on both PFD s, b) Destination and alternate airports have either LPV, GPS or FMS overlay approaches available without NOTAM restrictions for aeroplanes not equipped with Enhanced Navigation Package, c) Destination and alternate airports have either LPV, GPS, FMS overlay, or ILS approach available without NOTAM restrictions for aeroplanes equipped with Enhanced Navigation Package, d) No other display system failures exist, e) Associated Display Controller circuit breaker is pulled and collared, f) Alternate procedures are established and used, and g) Repairs are made within two (2) flight days. Maintenance will pull and collar associated Display Control circuit breaker. Flight crew will verify the required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable. When weather conditions exist at the destination or alternate airport during the approach, the PNF will be prepared to announce approach minimums in the event the operative Display Controller fails en route. be placed on the Right Side Display Controller and will be noted on

186 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 34. NAVIGATION 50. Synthetic Vision *** Primary Flight Display (SV-PFD) Functions D 2 0 be displayed in a prominante 51. DDA (Digital to *** Discrete Adapter) (GV only) 52. GNSSU WAAS (Wide *** Area Augmentation System or SBAS Space Based Augentation System) Function D 2 0 May be inoperative provided approach minimums do not require its use. D 2 0 WAAS function may be inoperative provided en route and approach procedures do not require its use. be displayed in a prominante be displayed in a prominante *** 1) LPV Enable Switches (GV Only) C 2 0 May be inoperative provided approach procedurs do not require is used. 53. CAS Scroll Switches D 2 0 May be inoperative provided both CCD s are operative. be displayed in a prominante be displayed in a prominante

187 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 35-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: OXYGEN 1. Passenger Oxygen System and Supply 1) Automatic Deployment System MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: B 1 0 (O) May be inoperative provided: a) Flight is not conducted over an area where the Minimum En route Altitude is above 13,000 ft MSL, b) Both air conditioning packs operate normally, c) Pressurization system operates normally, d) Flight is conducted at or below FL 250, e) Portable oxygen units are provided for all crew members and for 10 percent of the passengers for half an hour (supplemental oxygen), and f) Passengers are appropriately briefed. B 1 0 (O) May be inoperative provided: a) Maximum altitude is limited to a pressure altitude of 10,000 ft MSL, b) All air-conditioning packs operate normally, c) All other components of the pressurization system operate normally, and d) Passengers are appropriately briefed. C 1 0 (O) May be inoperative provided: a) Maximum altitude is limited to 25,000 ft pressure altitude, and b) Aeroplane is able to descend within 4 minutes to a cabin pressure altitude of 13,000 ft at all points along the route to be flown. Flight crew will ensure the route of flight is not over terrain exceeding 13,000 ft elevation, and passengers are briefed in accordance with the dispatch configuration. Flight crew will ensure maximum altitude is limited to a pressure altitude of 10,000 ft MSL and passengers are briefed in accordance with the dispatch configuration. Flight crew will ensure aeroplane is operated pressurised at or below 25,000 ft. be placed on affected Oxygen Control Panel or Mask Unit and will be noted on Additionally, affected seats shall be blocked and placarded. be placed on affected Oxygen Control Panel or Mask Unit and will be noted on Additionally, affected seats shall be blocked and placarded. be placed on affected Oxygen Control Panel or Mask Unit and will be noted on Additionally, affected seats shall be blocked and placarded.

188 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 35-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 35. OXYGEN 2. Cabin Oxygen ON Warning System MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 May be inoperative provided: a) Cabin Altitude and Differential Pressure Indicators are operative, and b) Cabin Altitude Pressure Warning System is operative. C 1 0 (O) May be inoperative provide aeroplane is operated in unpressurised configuration. be placed above "ON" position on Oxygen Control Panel and will be noted on To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed above "ON" position on Oxygen Control Panel and will be noted on

189 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 35-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: 0a MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 05/17/ OXYGEN NOTE: Information regarding the oxygen system capabilities for each aeroplane can be found in the Aeroplane Flight Manual Supplement for Oxygen Systems. The following document number, G450/G350 GC41453M000, G550/G500 GC51453M004 or GV GC52712M001 are associated with the Oxygen Flight Manual Supplements however, each operator must verify that the document number is applicable to the particular aeroplane. EXAMPLE OF G550 OXYGEN SYSTEM: OXYGEN REQUIRED FOR DE-PRESSURIZATION AND CONTINUED CRUISE REQUIRED BOTTLE PRESSURE AT DISPATCH TIME NUMBER OF PASSENGERS (HR:MIN) CRUISE ALTITUDE (FT) : : : : : : : : : : : : : : : : : : : : : : : : : : : Based on pressure reading at 70ºF. Includes oxygen for three crewmembers breathing 100% oxygen for emergency descent plus two minutes. Normal dillution for remainder of flight. Increase oxygen required by 37 PSIG for each crewmember on oxygen at/above FL410 for each 60 minutes. Maximum system pressure is 1800 PSIG. Values in excess of 1800 are shown for interpolation purposes only.

190 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 35-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: OXYGEN MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: CAT.IDE.235 Oxygen Minimum Requirements for Supplemental Oxygen for Pressurised Aeroplanes SUPPLY FOR: DURATION AND CABIN PRESSURE ALTITUDE 1. Occupants of flight crew compartment seats on flight crew compartment duty (a) The entire flying time when the cabin pressure altitude exceeds ft. (b) The remainder of the flying time when the cabin pressure altitude exceeds ft but does not exceed ft, after the initial 30 minutes at these altitudes, but in no case less than: (1) 30 minutes supply for aeroplanes certified to fly at altitudes not exceeding ft; and (2) 2 hours supply for aeroplanes certified to fly at altitudes of more than ft. 2. Required cabin crew members (a) The entire flying time when the cabin pressure altitude exceeds ft, but not less than 30 minutes supply. (b) The remainder of the flying time when the cabin pressure altitude exceeds ft but does not exceed ft, after the initial 30 minutes at these altitudes % of passengers The entire flying time when the cabin pressure altitude exceeds ft, but in no case less than 10 minutes supply % of passengers The entire flying time when the cabin pressure altitude exceeds ft but does not exceed ft % of passengers The remainder of the flying time when the cabin pressure altitude exceeds ft but does not exceed ft, after the initial 30 minutes at these altitudes.

191 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 35-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ OXYGEN 3. Oxygen Service Panel Pressure Gauges 4. Portable Oxygen *** Dispensing Units (Bottle and Mask) 5. Oxygen Supply Warning Systems D 2 0 May be inoperative provided the associated cockpit gauge is operative and monitored. B - - Any in excess of those required by Operating Requirements may be inoperative or missing provided required distribution is maintained throughout aeroplane. NOTE: Any bottle not properly serviced is considered inoperative and should be removed. C 2 0 May be inoperative provided associated cockpit gauge is operative and monitored. be placed on Oxygen Service Panel Gauges and will be noted on

192 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 35-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: OXYGEN 6. Protective Breathing *** Equipment (PBE) 7. Electronic Equipment *** Rack Oxygen Pressure Gauges 8. Cockpit Oxygen Pressure Indications MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: D - - (M) Any in excess of that required may be inoperative or missing provided the inoperative PBE is placarded inoperative, removed from the installed location and placed out of sight so it cannot be mistaken for a functional unit. D - 0 May be inoperative provided cockpit gauges are operative. C - 0 May be inoperative provided: a) Oxygen Service Panel Pressure Gauges are operative and checked before every takeoff, and b) Crew Oxygen Off and Passenger Oxygen Off messages are not displayed on the CAS prior to every takeoff. 9. First Aid Oxygen D - - (M) Any bottle in excess of those required may be inoperative provided the inoperative equipment is placarded inoperative, removed from the installed location (if portable) and placed out of sight so it cannot be mistaken for a functional unit. Maintenance will ensure the inoperative PBE is removed from its installed location or placed out of sight. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will ensure the inoperative bottle is removed from its installed location (if portable) or placed out of sight. Flight crew may accomplish this task if properly qualified and authorised.

193 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 35-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ OXYGEN 10. High Landing Field *** Elevation Passenger Oxygen Controller High Altitude Switch (GV-SP/GIV-X) D 1 0 May be inoperative provided the maximum Landing Field Elevation does not exceed 14,500 feet. 1) High Altitude *** Switch Light (GV-SP/GIV-X) D 1 0 May be inoperative provided the switch position is verified to be depressed in whenever the Landing Field Elevation exceeds 14,500 feet.

194 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ PNEUMATIC 1. Bleed Air Systems (GV, GV-SP) 1) Pressurised Configuration (continued) B 2 1 (M) Except for ER operations, one may be inoperative provided: a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, and d) Aeroplane is operated in accordance with AFM Limitations. NOTE: Autothrottle will be inoperative with Isolation Valve OPEN. Maintenance will CLOSE inoperative Bleed Control Valve and electrically deactivate affected system. If failure occurs with 1) Right Bleed Air Control Valve: Select Right Bleed Air Valve OFF utilizing R Eng Bleed Air Switch and Pull R Bleed CONT Circuit Breaker (CB). 2) Left Bleed Air Control Valve: Select Left Bleed Air Valve OFF utilizing L Eng Bleed Air Switch and Pull Left Bleed CONT Circuit Breaker (CB). In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN. Refer to AMM chapter Flight crew may accomplish this task if properly qualified and authorised. be placed above the affected Bleed Air Control Switch and will be noted on

195 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ PNEUMATIC 1. Bleed Air Systems (cont d) (GV, GV-SP) 2) Unpressurised Configration (continued) C 2 0 (M)(O) Except for ER operations, may be inoperative provided: a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Aeroplane is not operated in forecast or known icing conditions, and c) Aeroplane is operated in accordance with AFM Limitations. Maintenance will ensure both Bleed Air Valves are CLOSED and deactivated electrically. Flight crew may accomplish this task if properly qualified and authorised. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed above the affected Bleed Air Control Switch(es) and will be noted on

196 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ PNEUMATIC 1. Bleed Air Systems (cont d) (GIV-X only) 1) Pressurised Configuration B 2 1 (M) Except for ER operations, may be inoperative provided: a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, d) Aeroplane is not operated in forecast or known icing conditions, and e) Aeroplane is operated in accordance with AFM Limitations. Maintenance will CLOSE associated Bleed Control Valve and electrically deactivate system. In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN. Refer to AMM chapter Flight crew may accomplish this task if properly qualified and authorised. be placed above both Bleed Air Control Switches and will be noted on NOTE: Autothrottle will be inoperative with Isolation Valve OPEN.

197 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 36. PNEUMATIC 1. Bleed Air Systems (cont d) (GIV-X only) 2) Unpressurised Configuration B 2 0 (M)(O) Except for ER operations, may be inoperative provided: a) Affected Valve(s) are verified CLOSED, and b) Aeroplane is not operated in known or forecast icing conditions, and c) Aeroplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolatin Valve OPEN. Maintenance will ensure all affected Valve(s) are verified CLOSED. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. be placed on affected Valve(s) and will be noted on Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft.

198 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ PNEUMATIC 1. Bleed Air Systems (cont d) (GIV-X only) 3) Pressurised Configuration (continued) B 2 1 (M) Except for ER operations, may be inoperative provided: a) Affected Valve is verified OPEN, b) All components of both HP Bleed Air Systems are operative, c) Both Environmental Control Systems (ECS) Packs are operative, d) Performance Computer is initialized with COWL ANTI-ICE selected ON for either takeoff or landing when COWL ANTI-ICE valve is pressurised, and e) Aeroplane is operated in accordance with AFM Limitations and Performance. Maintenance will CLOSE associated Bleed Control Valve and electrically deactivate system. In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN. Refer to AMM chapter Flight crew may accomplish this task if properly qualified and authorised. be placed above both Bleed Air Control Switches and will be noted on

199 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ PNEUMATIC 1. Bleed Air Systems (cont d) (GIV-X only) 4) Unpressurised Configuration B 2 0 (M) (O) Except for ER operations, may be inoperative provided: a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Aeroplane is not operated in forecast or known icing conditions, and c) Aeroplane is operated in accordance with AFM Limitations. NOTE: Autothrottle will be inoperative with Isolation Valve OPEN. Maintenance will ensure both Bleed Air Valves are CLOSED and deactivated electrically. Flight crew may accomplish this task if properly qualified and authorised. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft. be placed above the affected Bleed Air Control Switch(es) and will be noted on

200 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-7 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ PNEUMATIC 2. Bleed Air Hot Warning Systems 1) Pressurised Configuration (continued) B 2 1 (M) Except for ER operations, may be inoperative provided: a) Associated Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, d) Aeroplane is not operated in known or forecast icing conditions, and e) Aeroplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. Maintenance will CLOSE associated Bleed Control Valve and electrically deactivate system. In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN. Refer to AMM chapter Flight crew may accomplish this task if properly qualified and authorised. be placed above both Bleed Air Control Switches and will be noted on

201 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-8 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 36. PNEUMATIC 2. Bleed Air Hot Warning System (cont d) 2) Unpressurised Configuration C 2 0 (M)(O) Except for ER operations, may be inoperative provided: a) Associated Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF, b) Aeroplane is not operated in forecast or known icing conditions, c) Aeroplane is operated at or below 10,000 feet MSL, and d) Aeroplane is operated in accordance with AFM Limitations. Maintenance will ensure both Bleed Air Valves are CLOSED and deactivated electrically by verifying the capsules indicate OFF. Flight crew may accomplish this task if properly qualified and authorised. To operate the aeroplane unpressurised, select manual pressurisation and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight. Refer to AFM Section : Unpressurized Flight. be placed above both Bleed Air Control Switches and will be noted on Flight crew will check that there is sufficient oxygen for the duration of the flight above 10,000 ft.

202 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 36-9 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 36. PNEUMATIC MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ Isolation Valve C 1 0 (M) May be inoperative provided: a) Both Bleed Air Systems are operative, b) Both Environmental Control Systems (ECS) Packs are operative, c) Isolation Valve is electrically deactivated, d) Isolation Valve is verified CLOSED, and e) Aeroplane is operated in accordance with AFM Limitations. NOTE: Valve must be OPENED manually during left engine start. Maintenance will ensure BOTH Bleed Air System and Environmental Control System (ECS) Packs are operative. In addition, Isolation Valve is to be electrically deactivated and verified "CLOSED". Refer to AMM chapters and Flight crew may accomplish this task if properly qualified and authorised. be placed on Isolation Valve Switch and will be noted on 4. Bleed Air System Switch Capsule Lights C 4 0 May be inoperative provided Bleed Air System indications are available on the Synoptic display. be placed on Bleed Air System Switch Capsule Lights and will be noted on

203 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 38-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 38. WATER/WASTE 1. Potable Water Systems 2. Lavatory Waste Systems (continued) C - - (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, b) Associated system components are verified not to have leaks, and c) Passengers are advised of the inoperative water system. NOTE: Any portion of system that is operative may be used. C - - (M) May be inoperative provided: a) System is drained, and b) Procedures are established to ensure that system is not serviced. C - - (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks. NOTE: Any portion of system that is operative may be used. Maintenance will ensure appropriate procedures are established to deactivate applicable system components and verify that components do not have leaks. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will drain the system and placard the access door to prohibit servicing. Flight crew may accomplish this task if properly qualified and authorised. Maintenance will ensure appropriate procedures are established to deactivate applicable system components and verify that components do not have leaks. If maintenance is not available, flight crew may perform the procedure. Flight crew may accomplish this task if properly qualified and authorised. be placed on Portable Water System and will be noted on be placed on Portable Water System and will be noted on be placed on Lavatory Waste System and will be noted on

204 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 38-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 38. WATER/WASTE 2. Lavatory Waste Systems (cont d) C - - (M) Associated lavatory system(s) may be inoperative provided: a) Associated components are deactivated or isolated to prevent leaks, and b) Associated lavatory door(s) is secured CLOSED and placarded INOPERATIVE - DO NOT ENTER. NOTE: These provisos are not intended to prohibit inspections by crewmembers. Maintenance will ensure appropriate procedures are established to deactivate applicable system components. If maintenance is not available, flight crew may perform the procedure. Flight crew may accomplish this task if properly qualified and authorised. be placed on Lavatory Waste System and will be noted on 3. Lavatory Dump/Drain System 4. Vacuum Toilet Holding Tank Indicator C - - May be inoperative provided: a) Dump valve is secured in the CLOSED and LOCKED position, and b) System is checked for leaks before every flight. D 1 0 May be inoperative provided: a) Tank is verified to be serviced prior to the first flight of the day, and b) Tank is serviced after the last flight of the day.

205 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 45-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 45. CENTRAL MAINTENANCE COMPUTER 1) Maintenance Data Acquisition Unit (MDAU) (GV) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 D 1 0 2) Central Maintenance Computer (CMC) (GV-SP, GIV-X) C 1 0 May be inoperative provided all faults are recorded after each flight. C 1 0 (M) May be inoperative or missing provided: a) All faults are recorded after each flight, and b) The CMC module is replaced with an Airflow Blockage Module (ABM) if the CMC module is removed from the MAU. Maintenance will ensure that if the CMC module is removed for maintenance, it is replaced with an Air Blockage Module (ABM). Refer to AMM chapter

206 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 46-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NEW TECHNOLOGY 1. Electronic Flight Bag *** Systems (EFBs) *** 1) Class 1, 2 & 3 EFB The purpose of this entry is not to require inclusion of Class 1 & 2 EFBs in an operators MEL, but it is one means of controlling inoperative EFB equipment. Other means may also be agreed with the NAA. C - - (M)(O) May be inoperative provided alternate procedures are established and used where operating procedures are dependant upon the use of the affected EFB. NOTE: Any EFB function which operates normally may be used. Maintenance will ensure EFB is secured by an alternate means if necessary and the mounting device is secured or removed from aeroplane if necessary. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will establish alternate procedures to include using other means to acquire data through datalink, SATCOM or FliteFone, or over the VHF/HF radio. (continued)

207 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 46-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NEW TECHNOLOGY 1. Electronic Flight Bag *** Systems (EFBs) (cont d) 2) Class 2 EFB *** a) Mounting Device *** C - 1 (M) (O) Any in excess of one may be inoperative provided the affected EFB is secured by an alternate means. C - 0 (M) (O) May be inoperative provided: a) The associated EFB is used in accordance with Class 1 EFB stowage criteria, and b) Alternate procedures are established and used where operating procedures are dependent upon the use of the affected EFB. Maintenance will ensure EFB is secured by an alternate means and the mounting device is secured or removed from aeroplane if necessary. Maintenance will ensure EFB is secured by an alternate means and the mounting device is secured or removed from aeroplane if necessary. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will establish alternate procedures to include using other means to acquire data through datalink, SATCOM or FliteFone, or over the VHF/HF radio. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will establish alternate procedures to include using other means to acquire data through datalink, SATCOM or FliteFone, or over the VHF/HF radio.

208 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 46-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NEW TECHNOLOGY 1. Electronic Flight Bag *** Systems (EFBs) (cont d) 2) Class 2 EFB *** b) Data Connectivity *** C - 1 (M)(O) Any in excess of one may be inoperative provided an alternate means of data connectivity is used. Maintenance will ensure inoperative data connectivity line is secured or removed from aeroplane if necessary. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will establish alternate procedures to include using other means to acquire data through datalink, SATCOM or FliteFone, or over the VHF/HF radio. C - 0 (M)(O) May be inoperative provided alternate procedures are established and used where operating procedures are dependent upon the use of the affected EFB NOTE: Any EFB function which operates normally may be used. Maintenance will ensure inoperative data connectivity line is secured or removed from aeroplane if necessary. Flight crew will ensure that en route charts and terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft. Flight crew will establish alternate procedures to include using other means to acquire data through datalink, SATCOM or FliteFone, or over the VHF/HF radio.

209 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 46-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ NEW TECHNOLOGY 1. Electronic Flight Bag *** Systems (EFB) (cont d) 3) Power Connection *** For Class 1 and Class 2 EFB C - 1 (M) (O) Any in excess of one may be inoperative provided an alternate power source is available and can be used for the anticipated duration of use of the affected EFB. C - 0 (M) (O) May be inoperative provided an alternate procedures are established and used. Maintenance will deactivate the inoperative power source by taping over the outlet. Alternatively, the power cord for the EFB can be removed from the EFB and battery power used to power EFB without a power source. Maintenance will deactivate the inoperative power sources by taping over the outlets. Alternatively, the power cord for the EFB can be removed from the EFB and battery power used to power the EFB s. Flight crew will ensure that the EFB battery is fully charged prior to flight. Flight crew will monitor and manage battery duration during flight. Flight crew will ensure that the EFB battery is fully charged prior to flight. Flight crew will monitor and manage battery duration during flight.

210 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 49-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 49. AIRBORNE AUXILIARY POWER 1. Auxiliary Power Unit (APU) 2. APU EGT Indicators (EICAS and Overhead) 3. APU Tachometers (EICAS and Overhead) C 1 0 (O) Except for ER operations, may be inoperative provided: a) Both Engine Driven generators are operative, and b) Standby Electrical System is operative. Flight crew will ensure: a) BOTH Engine Driven Generators are operative. AFM, Section 2, Normal Procedure, After Starting Engines. b) Standby Electrical System is operative. (Same as a). be placed on APU "MASTER" Switch and will be noted on C 2 1 be placed on APU "MASTER" Switch and will be noted on C 2 0 (M) Except for ER operations, may be inoperative provided: a) APU is not operated, b) Both Engine Driven generators are operative, and c) Standby Electrical System is operative. Maintenance will ensure APU CONT circuit breaker is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. be placed on APU "MASTER" Switch and will be noted on C 2 1 be placed on APU "MASTER" Switch and will be noted on C 2 0 (M) E xcept for ER operations, may be inoperative provided : a) APU is not operated, b) Both Engine driven generators are operative, and c) Standby Electrical System is operative. Maintenance will ensure APU CONT circuit breaker is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. be placed on APU "MASTER" Switch and will be noted on

211 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 49-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ AIRBORNE AUXILIARY POWER 4. APU "READY" Light System C 1 0 May be inoperative provided APU is operated in accordance with AFM Limitations. be placed on APU "READY" Light and will be noted on 5. APU Remote Oil Quantity/Servicing System C 1 0 May be inoperative provided oil is checked before every flight. be placed on APU Oil Quantity Indication System and will be noted on 6. APU Oil Pressure *** Gauges 7. APU Oil Temperature *** Gauges 8. APU Fuel Pressure *** Gauges 9. APU Start Indicator Light D - 0 be placed on APU Oil Pressure Gauges and will be noted on D - 0 be placed on APU Oil Temperature Gauges and will be noted on D - 0 be placed on APU Fuel Pressure Gauges and will be noted on C 1 0 be placed on APU Start Indicator Light and will be noted on

212 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 49-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ AIRBORNE AUXILIARY POWER 10. APU Air Load Control Valve C 1 0 (M) May be inoperative provided valve is verified in CLOSED position. Maintenance will ensure APU Air Load Valve is verified in a CLOSED position by Butterfly Plate Shaft Indicator. Flight crew may accomplish this task if properly qualified and authorised. 11. APU External Fire Warning Alarm (Fire Warning Bell) C 1 0 May be inoperative provided APU operation is monitored in cockpit. 12. APU Air Inlet Door System C 1 0 (M) Except for ER operations, may be inoperative provided: a) APU Air Inlet door is secured fully CLOSED, b) APU is not operated, c) Both Engine Driven Generators are operative, and d) Standby Electrical System is operative. Maintenance will ensure Air Intake Door is secured fully CLOSED by visually verifying door is CLOSED and pulling and collaring the APU door actuator circuit breaker. Flight crew may accomplish this task if properly qualified and authorised. be placed on APU Control Panel and will be noted on

213 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 49-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ AIRBORNE AUXILIARY POWER 13. Bleed Air Augmentation Valve (GV, GV-SP) 14. Surge Control Valve (GV, GV-SP) 15. Ignition System Channels (GV, GV-SP) 16. EGT Thermocouple System (GV, GV-SP) C 1 0 (O) May be inoperative provided: a) APU startng is not attempted above FL350, and b) APU is operated in accordance with AFM Limitations. C 1 0 (O) Except for ER operations, may be inoperative provided: a) APU is restricted to ground use only at pressure altitude of 8000 ft. or below, b) Both Engine Generators are operative, and c) Standby Electrical System is operative. Flight crew will ensure APU will be operated in accordance with AFM, Section 1, Limitations, APU Operation. Successful airstart only below 35,000 ft. Flight crew will ensure APU is restricted to ground use only at P.A. < 8000 ft. be placed in a prominent be placed in a prominent C 2 1 C 2 1

214 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 49-5 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original 49. AIRBORNE AUXILIARY POWER 17. Temperature Resistance Bulb (T2) 18. Inlet Pressure Transmitter (P2) (GV, GV-SP) 19. RPM Speed Sensor Channels (GV, GV-SP) MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/2011 C 1 0 C 1 0 C APU Hour Meter C Oil Temperature (GV, GV-SP) C 1 0 May be inoperative provided aeroplane is operated in accordance with AFM Limitations.

215 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 49-6 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ AIRBORNE AUXILIARY POWER 22. Deprime Solenoid (GV, GV-SP) C 1 0 (M) May be inoperative provided aeroplane is operated in accordance with AFM Limitations. Maintenance will verify Deprime Solenoid is inoperative by reference to MDAU. Maintenance will visually check APU oil level and perform APU start, run and shutdown per AFM procedures. Flight crew may accomplish this task if properly qualified and authorised. 23. Oil Heater (GV, GV-SP) C 1 0 May be inoperative provided aeroplane is operated in accordance with AFM Limitations. 24. APU Start/Engine *** Cowl Interrupt System D 1 0

216 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 52-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ DOORS 1. Door Warning Light System C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED by: a) Door latches or lock handles are flush, and b) Door edges are flush with fuselage. Flight crew will visually inspect Door(s) to ensure they are CLOSED and LOCKED prior to departure by ensuring that door latches or lock handles are flush and door edges are flush with fuselage. AFM, Section 2, Normal Procedures, After Starting Engines. 2. Cargo Door Operating *** System C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED by: a) Bayonets are visually confirmed to be in the locked position, and b) Door handle is in the stowed position. Maintenance will OPEN and CLOSE doors for each flight from outside aeroplane. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will ensure by visual inspection associated Door is CLOSED and LOCKED before each departure. In addition, flight crew will ensure door is OPENED and CLOSED by maintenance ground crew. be placed Externally and Internally near door operating handles and will be noted on 3. Cargo Door Warning *** Light System C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED by: a) Bayonets are visually confirmed to be in the locked position, and b) Door handle is in the stowed position. Maintenance will OPEN and CLOSE doors for each flight from outside aeroplane. Flight crew may accomplish this task if properly qualified and authorised. Flight crew will ensure by visual inspection associated Door is CLOSED and LOCKED before each departure. In addition, flight crew will ensure door is OPENED and CLOSED by maintenance ground crew.

217 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 52-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 52. DOORS 4. Door Seal Pressure *** Indicator D Main Entry Door Normal Operating System C 1 0 (O) May be inoperative provided: a) Alternate system is operative, and b) Main door is not CLOSED manually. Flight crew will select the AUX Hydraulic Pump ON, manually OPEN the door control valve, CLOSE and LOCK the main door, and manually CLOSE the door control valve. Refer to AOM Volume 3 Handling and Servicing Procedures. Section 9 item Main Entry Door Acoustic Curtain/ Door System D - 0 May be inoperative provided the affected curtain/door system is in the stowed position. 7. Lavatory Door D - 0 May be inoperative provided the affected door is secured OPEN or CLOSED for taxi, takeoff and landing. NOTE: Includes pop-up panels, latches, locks and handles. be placed on the Lavatory Door and will be noted on

218 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 52-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 52. DOORS 8. Baggage Door Warning System 9. Main Entry Door Warning System 10. Internal Baggage Door Warning System (GV, GV-SP) Internal Baggage Door Warning System (GIV-X) C 1 0 (O) May be inoperative provided a crewmember verifies by visual inspection before each departure that the baggage door is CLOSED and LOCKED by: a) Bayonets are visually confirmed to be in the locked position, and b) Door handle is in the stowed position. C 1 0 (O) May be inoperative provided a crewmember verifies by visual inspection before each departure that the Main Entry Door is CLOSED and LOCKED by: a) Bayonets are visually confirmed to be in the locked position, and b) Door handle is in the stowed position. C 1 0 (O) May be inoperative provided: a) Door is verified to be CLOSED and LOCKED by a crewmember after each use, and b) Door is placarded DO NOT ENTER above 40,000 ft. C 1 0 (O) May be inoperative provided: a) Baggage door is in CLOSED position, and b) Smoke detector is operative. C 1 0 (O) May be inoperative in the OPEN position provided baggage compartment is empty. Flight crew will ensure by visual inspection that baggage door is closed and locked before each departure. In addition, flight crew will ensure baggage door is opened and closed by maintenance ground crew. Flight crew will ensure by visual inspection that main entry door is closed and locked before each departure. In addition, flight crew will ensure main entry door is opened and closed by maintenance ground crew. Flight crew advises the passengers when the aeroplane is at or above 40,000 ft and that access to the baggage compartment is not allowed. Flight crew will test the smoke detector prior to the first flight of the day. Flight crew ensures that the baggage compartment is empty.

219 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 52-4 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: DOORS MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 11. Internal Pocket Doors D - - May be inoperative provided the affected door is secured OPEN for taxi, takeoff and landing. 12. Cabin Over Wing Exit Window Warning System NOTE: Includes pop-up panels, latches, locks and handles. C 1 0 May be inoperative provided a crewmember verifies by visual inspection before each departure that the cabin exit window internal and external locking (T) handles in the over wing access panels are engaged in their LOCKED position.

220 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 71-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ POWERPLANT 1. EPA Tank Ejector Pump D 2 0 (M) May be inoperative provided maintenance procedures are established to drain tank: a) Before the first flight of each day, b) After three normal shutdowns, and c) After two false (wet) starts. Maintenance will perform procedures in accordance with AMM Chapter If maintenance is not available, flight crew may perform the procedure.

221 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 73-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ ENGINE FUEL & CONTROL 1. Fuel Flow Indication Systems 1) EICAS C 2 1 May be inoperative provided: a) Associated EPR, LP and HP indicating systems are operative, and b) Fuel Quantity indicating systems are operative. 2) RFMU (GV) / MCDU (GV-SP)/ (GIV-X) 2. Fuel Low Pressure Warning Systems (EICAS) C 2 1 May be inoperative provided: a) Associated EPR, LP and HP indicating systems are operative, and b) Fuel Quantity indicating systems are operative. C 2 1 May be inoperative provided: a) Associated Fuel Boost Pumps are operative, and b) Aeroplane is operated at or below FL 250.

222 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 73-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ ENGINE FUEL & CONTROL 3. Engine FADEC Systems (GV, GV-SP) A 2 0 (M) (O) Aeroplane may be dispatched with Blue Engine Maintenance STD (###) and/or Engine Maintenance LTD messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), chapter 5 (no extensions are authorised), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: GV, GV-SP Blue Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue Engine Maintenance LTD messages required maintenance action within 500 hours. Maintenance will ensure repairs are made in accordance with times (hours) established by the BR710 Type Certificate Data Sheet. The times (hours) established for Engine Maintenance LTD (Long Term Dispatch) message is 500 engine hours. The times (hours) established for Engine Maintenance ### STD (Short Term Dispatch where ### is the number of hours remaining) is 150 engine hours when the fault is first logged. The hours remaining to affect the repair are automatically decreased by the system as engine time is accumulated. When the time remaining is zero, the fault automatically becomes a DND (Do Not Dispatch) fault. Flight crew will review the FADEC faults prior to each takeoff. Flight crew may accomplish this task if properly qualified and authorised. (continued)

223 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 73-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ ENGINE FUEL & CONTROL 3. Engine FADEC Systems (cont d) Engine FADEC System (GIV-X) A 2 0 (M) (O) Aeroplane may be dispatched with Blue Engine Maintenance STD (###) and/or Engine Maintenance LTD messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the Tay 611-8C Time Limits Manual, chapter 5 (no extensions are authorised), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: GIV-X Blue Engine Maintenance STD (###) message require maintenance action within 150 hours and Blue Engine Maintenance LTD messages required maintenance action within 500 hours. Maintenance will ensure repairs are made in accordance with times (hours) established by the Tay 611-8C Time Limits Manual, chapter 5. The times (hours) established for Engine Maintenance LTD (Long Term Dispatch) message is 500 engine hours. The times (hours) established for Engine Maintenance ### STD (Short Term Dispatch where ### is the number of hours remaining) is 150 engine hours when the fault is first logged. The hours remaining to effect the repair are automatically decreased by the system as engine time is accumulated. When the time remaining is zero, the fault automatically becomes a DND (Do Not Dispatch) fault. Flight crew will review FADEC faults prior to each takeoff. Flight crew may accomplish this task if properly qualified and authorised.

224 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 74-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: IGNITION 1. Ignition Systems MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 1) No. 1 Igniters A 2 1 One may be inoperative provided: a) Both No. 2 Igniters are operative, b) Takeoff runway does not have standing water, slush, or snow, and c) Repairs are made within 150 flight hours. A 2 0 May be inoperative provided: a) Both No. 2 Igniters are operative, b) Takeoff runway does not have standing water, slush, or snow, and c) Repairs are made within 10 flight days. 2) No. 2 Igniters A 2 1 One may be inoperative provided: a) Both No. 1 Igniters are operative, b) Takeoff runway does not have standing water, slush, or snow, and c) Repairs are made within 150 flight hours. A 2 0 May be inoperative provided: a) Both No. 1 Igniters are operative, b) Takeoff runway does not have standing water, slush, or snow, and c) Repairs are made within 10 flight days.

225 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 74-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ IGNITION 2. Ignition ON Indicator Systems C 2 0 (M) May be inoperative provided both airstart systems are verified to be operative before each flight. To check the igniters: Pull the IGN L/R #2 breaker. Select L & R airstart ignition switches ON. Verify igniters firing at the engines. Reset breakers. Pull IGN L/R #1 breaker. Select L & R airstart ignition switches ON. Verify igniters firing at the engines. Reset breaker when complete. be placed near affected Ignition "ON" Light and will be noted on

226 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 77-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 77. ENGINE INDICATING 1. HP Tachometer Indications EICAS C 2 1 May be inoperative on either engine provided associated LP, EPR and Fuel Flow Indicating Systems (EICAS or Standby) are operative for affected engine. NOTE: Standby HP Indication may also be inoperative on both engines. 2. Engine Vibration Monitor Systems Sensors 1) Primary Sensors 2) Secondary Sensors C 2 0 May be inoperative provided associated secondary sensor system is operative. C 2 0 May be inoperative provided associated primary sensor system is operative.

227 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 77-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ ENGINE INDICATING 3. Standby Engine Instruments Indicating System (RFMU) (GV) C 1 0 May be inoperative provided: a) Associated EICAS indication is operative, and b) All channels of both DAUs are operative. NOTE: Individual standby indications may be inoperative provided associated EICAS indication is operative. See individual indications for other authorised configurations. 4. Standby Engine Instruments on Multifunction Control Display (MCDU) (GV-SP, GIV-X) 5. Engine Vibration Monitoring System C 1 0 May be inoperative provided associated EICAS indication is operative. B 1 0 May be inoperative provided: a) Both Ice Detection Systems are operative, b) Operations are not conducted in known or forecast icing conditions, and c) Crew reviews the Abnormal Procedures for engine vibration before each takeoff.

228 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 78-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: ENGINE EXHAUST MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 1. Thrust Reversers C 2 0 (M) May be inoperative provided: a) Affected Thrust Reverser is deactivated, stowed and LOCKED in forward thrust position, and b) Aeroplane is operated in accordance with AFM Limitations and Procedures. May be inoperative provided: a) Affected Thrust Reverser is deactivated, stowed, and LOCKED in forward thrust position. Refer to AMM chapter b) Aeroplane is operated IAW AFM Limitations and Procedures. NOTE: AFM Landing Distances are not impacted for dry runway, refer to AFM , but is affected in wet/contaminated runway conditions, refer to AOM

229 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 79-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 79. ENGINE OIL 1. Low Oil Pressure Warning System 2. Engine Oil Replenishment System 3. Impending Oil Filter Bypass Indications C 2 1 May be inoperative provided oil pressure indication for both engines is operative. D 1 0 A 2 1 (M) May be inoperative provided: a) Associated oil filter bypass pop up indicator is verified in normal (recessed) position before each engine start, b) The oil filter is changed every flight day or every 15 flight hours, whchever occurs first, c) The Master Chip Detectors are checked and verified to be free of all debris, d) Procedures are in place to ensure all other DND (Do Not Dispatch) messages are addressed before dispatch, and e) Repairs are made within three (3) flight days. NOTE: An amber Engine Maintenance Required message will still be displayed on the Crew Alerting System. Dispatch is allowed with this message displayed after complying with the required (M) procedure. Maintenance will ensure: a) Associated oil filter bypass pop up indicator is verified in normal (recessed) position before each engine start b) Affected engine s oil filter is replaced per AMM, c) Fault is confirmed to be on the indication system, and d) Procedures are in place to ensure all other DND (Do Not Dispatch) messages are addressed before dispatch.

230 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 79-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ ENGINE OIL 4. Oil Quantity Indication Systems (EICAS / Ground Service Control Panel) 5. Oil Filter Pressure Switch Fault Indications C 2 0 May be inoperative provided the engine oil quantity is verified on the engine oil quantity gauge before each engine start. C 2 0 (M) May be inoperative provided: a) Associated oil filter bypass pop up indicator is verified in normal (recessed) position before each engine start, b) Oil filter fault is not displayed in MDAU (GV) or CMC (GV-SP, GIV-X), c) Fault is confirmed to be on the indication system, and d) Procedures are in place to ensure all other DND (Do Not Dispatch) messages are addressed before dispatch. NOTE: An amber Engine Maintenance Required message will still be displayed on the Crew Alerting System. Dispatch is allowed with this message displayed after complying with the required (M) procedure. Maintenance will ensure associated oil filter bypass pop up indicator is verified in normal (recessed) position before each engine start. Flight crew may accomplish this task if properly qualified and authorised.

231 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 80-1 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ STARTING 1. Engine Starting Systems C 2 1 (M) (O) May be inoperative provided: a) Airstart Ignition System is operative, b) Start Valve has not failed in OPEN position, c) Start Valve is manually OPENED and CLOSED for engine starting, d) Airstart Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached selfsustaining speed, and e) Engine start is accomplished in accordance with AFM Engine Start Valve Fails To Open Procedure. Maintenance will ensure: a) Start Valve has not failed in OPEN position, b) Start Valve is manually OPENED and CLOSED for engine starting, c) Airstart (Continuous) Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached self sustaining speed, and d) The Airstart Ignition System is operative. The flight crew may perform this task if properly qualified and authorised. Flight crew will ensure: a) Start Valve has not failed in OPEN position. b) Start Valve is manually OPENED and CLOSED for engine starting. c) Airstart (Continuous) Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached selfsustaining speed. d) Engine Start is accomplished in accordance with AFM, Section 3, Abnormal Procedures, Engine Starting System. 2. Auto Start System C 2 0 May be inoperative provided: a) Alternate start system is operative, and b) AFM procedures for alternate engine start are used to start engines. position to be seen by the flight crew and will be noted on the

232 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 80-2 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: 1 MOP REV. NO.: 1 MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: MOP DATE: 80. STARTING 3. Start Valve Position Indications C 2 1 (M) May be inoperative provided: a) Start Valve has not failed in OPEN position as verified by visual means through an access panel, b) Ignition ON indication is operative during engine start, and c) Start Valve is verified CLOSED by visual means following engine start. C 2 1 (M) (O) May be inoperative provided: a) Airstart Ignition System is operative, b) Start Valve has not failed in OPEN position, c) Start Valve is manually OPENED and CLOSED for engine starting, d) Airstart Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached selfsustaining speed, and e) Engine start is accomplished in accordance with AFM Engine Start Valve Fails To Open Procedure. Maintenance will ensure: a) Start Valve has not failed in OPEN position, b) Airstart ignition is operative, c) Start Valve is manually OPENED and CLOSED for engine starting. The flight crew may perform this task if properly qualified and authorised. Maintenance will ensure: a) Start Valve has not failed in OPEN position, b) Start Valve is manually OPENED and CLOSED for engine starting, c) Airstart (Continuous) Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached self sustaining speed, and d) The Airstart Ignition System is operative. The flight crew may perform this task if properly qualified and authorised. Flight crew will comply with QRH procedures for Manually Overriding Starter Air Valve OM found under Alternate Normal Procedures tab. be placed on Start Valve Position Indicator and will be noted on be placed on Start Valve Position Indicator and will be noted on

233 EUROPEAN AVIATION SAFETY AGENCY PAGE NUMBER: 80-3 AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-V, GV-SP (G550, G500), GIV-X (G450, G350) MMEL REV. NO.: Original MOP REV. NO.: Original MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL DATE: 01/28/2011 MOP DATE: 01/28/ STARTING 4. Start Valve C *** Position Indicator Lights 2 0 (M) May be inoperative provided: a) Start Valve has not failed in OPEN position as verified by visual means through an access panel, b) Start Valve is manually OPENED and CLOSED for engine starting in accordance with AFM Start Valve Failure procedures, and c) Airstart Ignition, Engine Selector and Start switches are switched to the OFF position when engine has reached self-sustaining speed. Maintenance will ensure a) Start Valve has not failed in OPEN position, b) Start Valve is manually OPENED and CLOSED for engine starting, c) Airstart (Continuous) Ignition, Engine Selector and Start Switches are switched to OFF when engine has reached self sustaining speed, and d) The Airstart Ignition System is operative. be placed on Start Valve Position Indicator Lights and will be noted on The flight crew may perform this task if properly qualified and authorised.

234 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: PAGE NO: 2-1 SECTION TWO CREW ALERTING SYSTEM (CAS) MESSAGE RELIEF

235 AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: PAGE NO: INTRODUCTION The following section has been authorized as an alternative to the standard method of MMEL dispatch relief, as is normally achieved through fault isolation procedures, and subsequent dispatch under LRU/Component MMEL relief. Section 2, herein, has been developed with the with the objective of allowing flight crews to dispatch from the displayed CAS (Crew Alerting System) message, without specifically identifying associated failed LRUs or components. As Section 2 is intended as an alternative dispatch relief methodology, the LRU/Component relief (Section 1) will be retained in order to provide maximum flexibility for relief. Flight crews / operators may dispatch failures with reference to either Section 1 or Section 2 of this MMEL to the advantage that either may provide. Upon comparison, it may be recognized in many cases that when comparing dispatch relief provisos for posted CAS messages to those of the related LRU / Component dispatch relief, the provisos associated with the CAS message will generally be more restrictive in content and relief interval. Without the opportunity for fault isolation through maintenance, it must be assumed that worst-case failure conditions always underlie the posted message - commensurately, dispatch should be more restrictive. However, where maintenance personnel are available and fault isolation conducted, relief provisos in Section 1 may be found to provide fewer or less stringent restrictions upon operations and offer a longer relief interval. Section 2 has been arranged in alphabetical order of the indicated CAS message, without association to ATA Chapter. However, to avoid any possible mis-identification, each message is identified beneath as to its alert level. Repair intervals (A, B, C & D) associated with CAS message reliefs herein, remain consistent with those of Section 1, and as described in the Definitions section in the front matter of this MMEL. In conjunction with Section 2, a new separate dispatch procedures section has also been developed, also arranged in alphabetical order of the indicated CAS message. Where deemed necessary, the familiar (O) indicates the need for such supporting tasks. Acceptable tasks include, but are not necessarily limited to the following duties: a) Procedures described which exercise cockpit (or cabin) system controls utilized in normal flight operations; b) Deactivation of affected systems, as achieved by pulling system breaker or use of remote electronic system isolation; c) Visual inspection behind panels (internal or external) which are accessible without tools via quick-release latches and which clearly indicate their unlocked or unsafe state;(red/green safe window; flush fit latches) (candidates to be verified at FOEB) d) Visual confirmation of remote gauge indications, or valve positions as provided by integral external indicators. 2-2

236 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message A/P TRIM PWR FAIL (Blue Advisory) (GV) A/T 1-2 FAIL (Blue Advisory) A/T 1-2 TQA Power Fail (Blue Advisory) (GV-SP/GIV-X) ACS Default Mode, L-R (Blue Advisory) (GV-SP/GIV-X) ACS DEFLT MODE, L-R (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched with one (1) elevator trim servo inoperative provided the affected IAC #1 POP, D-8 or IAC #2, CPOP, D-8 inoperative trim servo circuit breaker is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. B (O) Aeroplane may be dispatched provided affected A/T system is confirmed disengaged. B (O) Aeroplane may be dispatched provided affected A/T system is confirmed disengaged. C Aeroplane may be dispatched. C Aeroplane may be dispatched. PAGE NO: Operational Procedures Flight crew will ensure affected IAC #1 POP, D-8 or IAC #2, CPOP, D-8 inoperative trim servo circuit breaker is pulled and collared. Fligth crew will confirm affected A/T system is disengaged. Fligth crew will confirm affected A/T system is disengaged.

237 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ACS Fail, L-R (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Except for ER operations, aeroplane may be dispatched in the pressurized configuration with a single pack inoperative provided: a) Inoperative ECS Pack is selected OFF, b) Bleed Air Isolation Valve is CLOSED and OPERATIVE, c) Right Main TRU is operative, d) Aeroplane is operated in accordance with AFM Limitations, e) Aeroplane is operated at or below FL410, and f) Autothrottles must be operative and engaged at or above FL400. B Except for ER operations, aeroplane may be dispatched in the unpressurized configuration with both packs inoperative and selected OFF provided the outflow valve is operative. PAGE NO: Operational Procedures

238 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ACS FAIL, L-R (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Except for ER operations, aeroplane may be dispatched in the pressurized configuration with a single pack inoperative provided: a) Inoperative ECS Pack is selected OFF, b) Bleed Air Isolation Valve is CLOSED and OPERATIVE, c) Right Main TRU is operative, d) Aeroplane is operated in accordance with AFM Limitations, e) Aeroplane is operated at or below FL410, and f) Autothrottles must be operative and engaged at or above FL400. B Except for ER operations, aeroplane may be dispatched in the unpressurized configuration with both packs inoperative and selected OFF provided the outflow valve is operative. PAGE NO: Operational Procedures

239 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ACS Maintenance, L-R (Blue Advisory) (GV-SP/GIV-X) ACS MAINT REQD, L-R (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, and d) Autopilot is operative. C (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, and d) Autopilot is operative. PAGE NO: Operational Procedures Flight crew will ensure: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, and d) Autopilot is operative. Flight crew will ensure: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, and d) Autopilot is operative.

240 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ADF 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) ADM1-3 Probe Heat Fail (Blue Advisory) (GV-SP) ADM2 Stby Probe Heat Fail (Blue Advisory) (GV-SP) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched provided system is not required by Operating Requirements. A (O) Except for ER operations, aeroplane may be dispatched with one (1) probe heater inoperative provided: a) Aeroplane is not operated in visible moisture or known or forecast icing conditions, b) Flight crew select ADS sources that are different and not associated with failed pitot heater element, and c) Repairs are made within two (2) flight days. A (O) Except for ER operations, aeroplane may be dispatched with one (1) probe heater inoperative provided: a) Aeroplane is not operated in visible moisture or known or forecast icing conditions, b) Flight crew select ADS sources that are different and not associated with failed pitot heater element, c) Dispatch in conjuction with ADM 1-3 Probe Heat Fail is prohibited, and d) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will select ADS sources that are different and not associated with failed pitot heater element and transfer transponder to an operable ADM Flight crew will select ADS sources that are different and not associated with failed pitot heater element

241 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ADS 1-2 Probe Heat Fail (Blue Advisory) (GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched with one (1) probe heater inoperative provided: a) Aeroplane is not operated in visible moisture or known or forecast icing conditions, b) Flight crew select ADS sources that are different and not associated with failed pitot heater element, and c) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will select ADS sources that are different and not associated with failed pitot heater element.

242 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ADS Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched with a single air data system inoperative provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations, f) ADM #1: POP B-8, ADM #2: CPOP B-8 and ADM #3: POP B-9 circuit breaker associated with ADS failure is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and g) Flight crew selects operative and different ADS sources prior to departure. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: Transponder and Flight Director / Autopilot must use same ADC data for RVSM. NOTE 3: For ADS 1 Fail, expect the L Engine Backup Air Data advisory and associated Engine Maintenance message to post. NOTE 4: For ADS 2 Fail, expect the R Engine Backup Air Data advisory and associated Engine Maintenance message to post. PAGE NO: Operational Procedures Flight crew will pull and collar the ADM #1: POP B-8, ADM #2: CPOP B-8 and ADM #3: POP B- 9 circuit breaker associated with the ADS failure.

243 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ADS 3 Stby Probe Heat Fail (Blue Advisory) (GIV-X) ADS-B Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched with one (1) probe heater inoperative provided: a) Aeroplane is not operated in visible moisture or known or forecast icing conditions, b) Flight crew selects ADS sources that are different and not associated with failed pitot heater element, c) Dispatch in conjuction with ADM 1-2 Probe Heat Fail is prohibited, and d) Repairs are made within two (2) flight days. NOTE: Standby instruments and ADS 3 may be unreliable. D Aeroplane may be dispatched provided operations do not require its use. PAGE NO: Operational Procedures Flight crew will select ADS sources that are different and not associated with failed pitot heater element.

244 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Aft Cabin Temp Fan Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: Forward Cabin Temp Fan Fail; Cockpit Temp Fan Fail; b) Aft Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) AFT CABIN SENSOR FAN, LEER E-9, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and e) Flight crew monitor aft cabin temperature and aft cabin duct temperature. PAGE NO: Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: Forward Cabin Temp Fan Fail; Cockpit Temp Fan Fail, b) Aft Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) AFT CABIN SENSOR FAN circuit breaker: LEER E-9 is pulled and collared, and e) Aft cabin temperature and aft cabin duct temperature are monitored.

245 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message AFT CABIN TMP FAN FL (Blue Advisory) (GV) AGM DMU Charts Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: Forward Cabin Temp Fan Fail; Cockpit Temp Fan Fail; b) Aft Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) AFT CABIN SENSOR FAN, LEER E-9, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and e) Flight crew monitor aft cabin temperature and aft cabin duct temperature. C Aeroplane may be dispatched provided: a) Current aeronautical charts are carried onboard the aeroplane and available to the flight crew, and b) Aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: Forward Cabin Temp Fan Fail; Cockpit Temp Fan Fail, b) Aft Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) AFT CABIN SENSOR FAN circuit breaker: LEER E-9 is pulled and collared, and e) Aft cabin temperature and aft cabin duct temperature are monitored.

246 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message AGM Fail (Blue Advisory) (GV-SP/GIV-X) AIU 1-2 FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched with one AGM inoperative provided: a) The inoperative AGM is electronically switched to the AGM 3 position resulting in DU3 red Xing, b) DU3 is dimmed to eliminate the Red X, and c) Crew actions for subsequent failures are established. A Aeroplane may be dispatched with one AIU inoperative provided: a) Operations do not require use of HF radio, and b) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure: a) The inoperative AGM is electronically switched to the number 3 position resulting in DU3 red Xing, b) DU 3 is dimmed to eliminate the Red X, and c) Crew actions for subsequent failures are established

247 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Alternate Pump Fail, L-R (Amber Caution) (GV-SP) Alt FuelPump Fail, L-R (Amber Caution) (GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with a single pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and e) Aeroplane is operated in accordance with AFM Limitations. B (O) Except for ER operations, aeroplane may be dispatched with a single pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and e) Aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, and c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure. Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, and c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure.

248 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ALT PUMP FAIL, L-R (Amber Caution) (GV) Antiskid Fail (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with a single pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and e) Aeroplane is operated in accordance with AFM Limitations. B (O) Aeroplane may be dispatched provided: a) ANTI-SKID is selected OFF, b) Anti-skid off braking procedures, AFM Section 3, Abnormal Procedures, Anti-Skid Failure are followed, c) No WOW Power Faults exist, d) If Auto mode of the AUX Hydraulic Pump is inoperative, AUX pump is selected ON for takeoff and landing, and e) Aeroplane is operated in accordance with AFM Limitations. NOTE: Anti-Skid inoperative AFM performance penalties must be applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance. PAGE NO: Operational Procedures Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, and c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure Flight crew will ensure airplane is operated in accordance with AFM, Limitations. Flight crew will select ANTI-SKID OFF and follow Anti-Skid Off Braking Procedures. AFM, Section 3, Abnormal Procedures, Anti-Skid Failure. NOTE: May be inoperative provided AFM performance penalties are applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance.

249 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ANTISKID FAIL (Amber Caution) (GV) AP 1-2 Fail (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched provided: a) ANTI-SKID is selected OFF, b) Anti-skid off braking procedures, AFM Section 3, Abnormal Procedures, Anti-Skid Failure are followed, c) No WOW Power Faults exist, d) If Auto mode of the AUX Hydraulic Pump is inoperative, AUX pump is selected ON for takeoff and landing, and e) Aeroplane is operated in accordance with AFM Limitations. NOTE: Anti-Skid inoperative AFM performance penalties must be applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance. B (O) Except for ER operations or where en route operations or approach minimums require its use, Aeroplane may be dispatched with one (1) Autopilot inoperative provided the aeroplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative. NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations. PAGE NO: Operational Procedures Flight crew will ensure airplane is operated in accordance with AFM, Limitations. Flight crew will select ANTI-SKID OFF and follow Anti-Skid Off Braking Procedures. AFM, Section 3, Abnormal Procedures, Anti-Skid Failure. NOTE: May be inoperative provided AFM performance penalties are applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance. Flight crew will operate the airplane in accordance AFM limitations in the event the operative FGC fails and the Yaw Damper is inoperative

250 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message AP 1-2 Power Fail (Blue Advisory) (GV-SP/GIV-X) AP/Trim Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations or where en route operations or approach minimums require its use, Aeroplane may be dispatched with one (1) inoperative provided aeroplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative. NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations. B (O) Aeroplane may be dispatched with one (1) elevator trim servo inoperative provided the inoperative trim servo circuit breaker(s) is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. PAGE NO: Operational Procedures Flight crew will operate airplane in accordance with AFM limitations in the event the FGC fails and the Yaw Damper is inoperative. GV-SP: Flight crew will ensure inoperative PITCH TRIM SERVO #1: POP, E-2 or PITCH TRIM SERVO #2: CPOP, E-1 servo circuit breaker is pulled and collared. GIV-X: Flight crew will ensure inoperative PITCH TRIM SERVO #1: POP, E-2 or PITCH TRIM SERVO #2: CPOP, E-1 servo circuit breaker is pulled and collared.

251 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message APM Fail (Blue Advisory) (GV-SP/GIV-X) APU Fail (Amber Caution) (GV-SP/GIV-X) APU FAIL (Amber Caution) (GV) APU Fire Bottle Discharge (Amber Caution) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched with one (1) APM inoperative. B (O) Except for ER operations, aeroplane may be dispatched provided: a) Both Engine Driven generators are operative, and b) Standby Electrical System is operative. B (O) Except for ER operations, aeroplane may be dispatched provided: a) Both Engine Driven generators are operative, and b) Standby Electrical System is operative. B (O) Except for ER operations, aeroplane may be dispatched provided: a) APU is considered inoperative, b) Both engine driven generators are operative, c) Standby electrical system is operative, and d) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. PAGE NO: Operational Procedures Flight crew will ensure: a) BOTH Engine Driven Generators are operative, and b) Standby Electrical system is operative. Flight crew will ensure: a) BOTH Engine Driven Generators are operative, and b) Standby Electrical system is operative. Flight crew will pull and collar APU CONT #1 and APU CONT #2 circuit breaker and will ensure: a) Both Engine Generators are operative, and b) Standby Electrical Power System is operative.

252 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message APU Fire Detector Fail (Amber Caution) (GV-SP/GIV-X) APU FIRE DET FAIL (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched provided: a) APU is not used, and b) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. B (O) Except for ER operations, aeroplane may be dispatched provided: a) APU is not used, and b) APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. PAGE NO: Operational Procedures Flight crew will ensure APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared. Flight crew will ensure APU CONT #1 and APU CONT #2 circuit breakers are pulled and collared.

253 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message APU GCU Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and c) Standby Electrical System is operative.

254 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message APU GCU FAIL (Blue Advisory) (GV) APU Generator Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. A (O) Except for ER operations, aeroplane may be dispatched provided: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and c) Standby Electrical System is operative. Flight crew will ensure: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and c) Standby Electrical System is operative

255 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message APU Generator Maint Reqd (Blue Advisory) (GV-SP/GIV-X) APU GEN FAIL (Blue Advisory) (GV) APU GEN MAINT REQD (Blue Advisory) (GV) APU Maintenance Required (Blue Advisory) (GV-SP/GIV-X) APU MAINT REQD (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C Aeroplane may be dispatched. A (O) Except for ER operations, aeroplane may be dispatched provided: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. C Aeroplane may be dispatched. C Aeroplane may be dispatched. C Aeroplane may be dispatched. PAGE NO: Operational Procedures Flight crew will ensure: a) APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared, b) BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and c) Standby Electrical System is operative.

256 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message APU Shutoff Valve Fail (Amber Caution) (GV-SP/GIV-X) ATC 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, may be inoperative provided: a) Both Engine Driven generators are operative, b) Standby Electrical System is operative, c) APU CONT #1 LEER C-13 and APU CONT # 2 REER C-11 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and d) APU is not used. C Aeroplane may be dispatched with either transponder failed in excess of those required by Operating Requirements. NOTE 1: Flight Director, Autopilot, and Transponder must use the same Air Data source for flight into RVSM airspace. NOTE 2: Transponder and altitude reporting capability must be operative for flight into RVSM airspace. PAGE NO: Operational Procedures Flight crew will ensure: a) BOTH Engine Driven Generators are operative, b) Standby Electrical system is operative, and c) Pull and collar the APU CONT #1 LEER C-13 and APU CONT # 2 REER C-11 circuit breakers to ensure that the APU cannot be used in flight

257 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAROSET 1 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: 1. ADS 2 Fail 2. ADS 3 Fail 3. BAROSET 2 Fail 4. BAROSET 3 Fail b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Aeroplane is operated in accordance with AFM Limitations. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: Transponder and Flight Director/Autopilot must use same ADC data for RVSM. PAGE NO: Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: 1. ADS 2 Fail 2. ADS 3 Fail 3. BAROSET 2 FAIL 4. BAROSET 3 FAIL b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Airplane is operated in accordance with AFM Limitations

258 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAROSET 2 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: 5. ADS 1 Fail 6. ADS 3 Fail 7. BAROSET 1 Fail 8. BAROSET 3 Fail b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Aeroplane is operated in accordance with AFM Limitations. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: Transponder and Flight Director/Autopilot must use same ADC data for RVSM. PAGE NO: Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: 1. ADS 1 Fail 2. ADS 3 Fail 3. BAROSET 1 FAIL 4. BAROSET 3 FAIL b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Airplane is operated in accordance with AFM Limitations

259 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAROSET 3 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: 1. ADS 1 Fail 2. ADS 2 Fail 3. BAROSET 1 Fail 4. BAROSET 2 Fail b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Aeroplane is operated in accordance with AFM Limitations. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: Transponder and Flight Director/Autopilot must use same ADC data for RVSM. PAGE NO: Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: 1. ADS 1 Fail 2. ADS 2 Fail 3. BAROSET 1 FAIL 4. BAROSET 2 FAIL b) Manual Pressurization Control System is operative, c) Cabin Altitude and Differential Pressure Indicators are operative, d) Cabin Rate of Climb Indicator is operative, e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure, f) Autopilot is operative, and g) Airplane is operated in accordance with AFM Limitations

260 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAS Default Mode, L-R (Blue Advisory) (GV-SP/GIV-X) BAS DEFLT MODE, L-R (Blue Advisory) (GV) BAS Fail, L-R (Amber Caution) (GV-SP/GIV-X) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C Aeroplane may be dispatched. C Aeroplane may be dispatched. B (O) Except for ER operations, aeroplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided (GV-SP): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, and d) Aeroplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. PAGE NO: Operational Procedures GV-SP pressurized configuration: Flight crew will CLOSE inoperative Bleed Control Valve and electrically deactivate affected system. If failure occurs with 1) Right Bleed Air Control Valve: Select Right Bleed Air Valve OFF utilizing R Eng Bleed Air Switch and pull R BLEED AIR CONT REER E-9 and R WING ANTI-ICE REER D-13 circuit breaker. 2) Left Bleed Air Control Valve: Select Left Bleed Air Valve OFF utilizing L Eng Bleed Air Switch and pull L BLEED AIR CONT: LEER E- 10 and L WING ANTI-ICE: LEER, D-4 circuit breaker. In addition, opposite Engine Bleed Air System will be verified operative and Isolation Valve will be selected OPEN.

261 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAS Fail, L-R (Amber Caution) (GV-SP/GIV-X) (cont d) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided (GIV-X): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, d) Aeroplane is not operated in forecast or known icing conditions, and e) Aeroplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. PAGE NO: Operational Procedures GIV-X pressurized configuration: Flight crew will CLOSE associated Bleed Control Valve and electrically deactivate affected system and pull and collar R BLEED AIR CONT: REER, E-9 and R WING ANTI- ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers. In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN

262 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAS Fail, L-R (Amber Caution) (GV-SP/GIV-X) (cont d) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided (GV-SP): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Manual pressurization control is selected, c) Outflow valve is slewed to the full OPEN position, d) RAM Air is selected ON, e) Cabin differential pressure is monitored to be nominally zero psid during the flight, f) Aeroplane is not operated in known or forecast icing conditions, and g) Aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures For GV-SP unpressurized configuration: Flight crew will ensure inoperative Bleed Control Valve is CLOSED and deactivated electrically and pull and collar R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

263 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAS Fail, L-R (Amber Caution) (GV-SP/GIV-X) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided GIV-X): a) Affected Valve(s) are verified CLOSED, b) Manual pressurization control is selected, c) Outflow valve is slewed to the full OPEN position, d) RAM Air is selected ON, e) Cabin differential pressure is monitored to be nominally zero psid during the flight, f) Aeroplane is not operated in forecast or known icing conditions, and g) Aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures For GIV-X unpressurized configuration: Flight crew will ensure all affected Valve(s) are verified CLOSED. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

264 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAS FAIL, L-R (Amber Caution) (GV) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided (GV): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D- 13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Opposite Engine Bleed Air System is operative, c) Isolation Valve is verified to be operative and selected OPEN, and d) Aeroplane is operated in accordance with AFM Limitations. NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN. PAGE NO: Operational Procedures GV pressurized configuration: Flight crew will CLOSE inoperative Bleed Control Valve and electrically deactivate affected system. If failure occurs with 1) Right Bleed Air Control Valve: Select Right Bleed Air Valve OFF utilizing R Eng Bleed Air Switch and Pull R Bleed CONT REER, E-9 and R WING ANTI-ICE: REER, D-13 circuit breakers. 2) Left Bleed Air Control Valve: Select Left Bleed Air Valve OFF utilizing L Eng Bleed Air Switch and Pull Left Bleed CONT LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers. In addition, opposite Engine Bleed Air System will be verified operative and Isolation Valve will be selected OPEN.

265 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAS FAIL, L-R (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided (GV): a) Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows: 1. Affected Bleed Air Valve is selected OFF 2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Manual pressurization control is selected, c) Outflow valve is slewed to the full OPEN position, d) RAM Air is selected ON, e) Cabin differential pressure is monitored to be nominally zero psid during the flight, f) Aeroplane is not operated in known or forecast icing conditions, and g) Aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures For GV unpressurized configuration: Flight crew will ensure both Bleed Air Valves are CLOSED and deactivated electrically and pull and collar R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

266 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message BAS Maintenance Reqd, L-R (Blue Advisory) (GV-SP/GIV-X) BAS MAINT REQD, L-R (Blue Advisory) (GV) BATT CHGR FAIL, L-R (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C Aeroplane may be dispatched. C Aeroplane may be dispatched. A (O) Aeroplane may be dispatched with one inoperative battery charger provided: a) Both Engine Generators are operative, b) APU Generator is operative, c) Associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, d) Standby Electrical System is operative, e) Affected Battery is selected OFF, and f) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar associated BATT CHGR circuit breakers: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box.

267 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Battery Charger Fail, L-R (Amber Caution) (GV-SP/GIV-X) Brake Maintenance Reqd (Blue Advisory) (GV-SP/GIV-X) BRAKE MAINT REQD (Blue Advisory) (GV) CAB PRESS SEMIAUTO (Blue Advisory) (GV) Cabin Pressure Semi-auto (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with one inoperative battery charger provided: a) Both Engine Generators are operative, b) APU Generator is operative, c) Associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, d) Standby Electrical System is operative, e) Affected Battery is selected OFF, and f) Repairs are made within two (2) flight days. C Aeroplane may be dispatched. C Aeroplane may be dispatched. C Aeroplane may be dispatched provided aeroplane is operated in accordance with AFM Limitations. C Aeroplane may be dispatched provided aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures Flight crew will ensure that associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared.

268 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CCD 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) CDU FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched provided: a) Both Display Controllers, Weather Radar Controllers, and 2 MCDU s are operative, and b) Current terminal charts for the origin, destination and alternate airports are carried onboard the aeroplane and available to the flight crew. A Except where en route operations or approach minimums require its use, aeroplane may be dispatched provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMUs are operative, and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. PAGE NO: Operational Procedures Flight crew will ensure: a) Both Display Controllers, Weather Radar Controllers and two MCDUs are operative, and b) Current terminal charts for the origin, destination and alternate airports are carried, or EFB s are carried, onboard the airplane and available to the flight crew.

269 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CHECKLIST MISMATCH (Blue Advisory) (GV) CKPT TEMP FAN FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched provided: a) The checklist module in Fault Warning Computer (FWC) 1 is operative, and b) Current paper checklists are utilized. C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail; b) Cockpit Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) CKPT SENSOR FAN, REER D-10, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and e) Flight crew monitor cockpit temperature and cockpit duct temperature. PAGE NO: Operational Procedures Flight crew will ensure: a) The checklist module in Fault Warning Computer (FWC) 1 is operative, and b) Utilize current paper checklists. Flight crew will ensure: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail, b) Cockpit Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) CKPT SENSOR FAN circuit breaker: REER D-10 is pulled and collared, and e) Cockpit temperature and cockpit duct temperature are monitored.

270 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CMC Fail (Blue Advisory) (GV-SP/GIV-X) CMF 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) CMS 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched provided all faults are recorded after each flight. B (O) Aeroplane may be dispatched provided: a) Alternate procedures are established and used, and b) Flight crew utilizes voice over VHF/HF to relay pertinent information to the air traffic management system. B (O) Aeroplane may be dispatch provided routine procedures do not require its use. B Aeroplane may be dispatched with one (1) system inoperative. PAGE NO: Operational Procedures Flight crew will ensure: a) Alternate procedures are established and used, and b) Voice over VHF/HF is used to relay pertinent information to the air traffic management system. Flight crew will ensure alternate procedures are established and used.

271 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Cockpit Temp Fan Fail (Blue Advisory) (GV-SP/GIV-X) Cockpit Voice Recorder Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail; b) Cockpit Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) CKPT SENSOR FAN, REER D-10, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and e) Flight crew monitor cockpit temperature and cockpit duct temperature. A One or more may be inoperative provided: a) Not more than 72 hours have elapsed since cockpit voice recorder was found to be unserviceable, b) Aeroplane does not exceed 8 further consecutive flights with cockpit voice recorder unserviceable, and c) Any flight data recorder required to be carried is operative. PAGE NO: Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail, b) Cockpit Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) CKPT SENSOR FAN circuit breaker: REER D-10 is pulled and collared, and e) Cockpit temperature and cockpit duct temperature are monitored.

272 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Cowl Valve Fail Open, L-R (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched with one (1) valve inoperative provided: a) Affected Valve is verified OPEN, b) All components of both HP Bleed Air Systems are operative, c) Both Environmental Control Systems (ECS) Packs are operative, d) Affected Cowl Anti-Ice switch is ON, e) Affected L COWL ANTI-ICE: LEER, D-3 or R COWL ANTI-ICE: REER, D-14 valve circuit breaker is pulled or in the OPEN position. Flight crew may accomplish this task if properly qualified and authorized, f) Performance Computer is initialized with COWL ANTI ICE selected ON for either takeoff or landing when COWL ANTI-ICE valve is pressurized, and g) Aeroplane is operated in accordance with AFM Limitations and Performance. PAGE NO: Operational Procedures Flight crew will ensure: a) BOTH HP Bleed Air Systems and BOTH Environmental Control System (ECS) Packs are operative, b) Select the affected Cowl Anti-Ice switch ON and ensure that the affected valve circuit breaker is pulled or in the OPEN position, and c) Flight crew verifies that fact by viewing the ECS synoptic page to see that Cowl Antiice pressure is indicated. There will also be an A/I icon in the TGT instrument

273 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message COWL VLV FL OP, L-R (Amber Caution) (GV) CPAM Fail (Amber Caution) (GV-SP/GIV-X) CPAM FAIL (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched with one (1) valve inoperative provided: a) Affected Valve is verified OPEN, b) All components of both HP Bleed Air Systems are operative, c) Both Environmental Control Systems (ECS) Packs are operative, d) Affected Cowl Anti-Ice switch is ON, e) Affected L COWL ANTI-ICE: LEER, D-3 or R COWL ANTI-ICE: REER, D-14 valve circuit breaker is pulled or in the OPEN position. Flight crew may accomplish this task if properly qualified and authorized, f) Performance Computer is initialized with COWL ANTI ICE selected ON for either takeoff or landing when COWL ANTI-ICE valve is pressurized, and g) Aeroplane is operated in accordance with AFM Limitations and Performance. B Aeroplane may be dispatched provided both CPCS automatic systems are operative. B Aeroplane may be dispatched provided both CPCS automatic systems are operative. PAGE NO: Operational Procedures Flight crew will ensure: a) BOTH HP Bleed Air Systems and BOTH Environmental Control System (ECS) Packs are operative, b) Select the affected Cowl Anti-Ice switch ON and ensure that the affected valve circuit breaker is pulled or in the OPEN position, and c) Flight crew verifies that fact by viewing the ECS synoptic page to see that Cowl Antiice pressure is indicated. There will also be an A/I icon in the TGT instrument

274 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations and Abnormal Procedures (for Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days PAGE NO: Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, and Section 3, Abnormal Procedures. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

275 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, and Section 3, Abnormal Procedures. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

276 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS 1-2 FAIL (Blue Advisory) (GV) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations and Abnormal Procedures (for Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days PAGE NO: Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, and Section 3, Abnormal Procedures. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

277 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS 1-2 FAIL (Blue Advisory) (GV) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Section 1, Limitations, and Section 3, Abnormal Procedures. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

278 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS Channel 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations and Abnormal Procedures (for Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Limitations, and Abnormal Procedures. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

279 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS Channel 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Limitations, and Abnormal Procedures. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

280 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS CHNL 1-2 FAIL (Blue Advisory) (GV) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations and Abnormal Procedures (for Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Limitations, and Abnormal Procedures. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

281 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS CHNL 1-2 FAIL (Blue Advisory) (GV) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items, e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate airplane in accordance with AFM, Limitations, and Abnormal Procedures. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

282 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS Control Panel Fail (Amber Caution) (GV-SP/GIV-X) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations (for Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

283 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS Control Panel Fail (Amber Caution) (GV-SP/GIV-X) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

284 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS CONT PNL FAIL (Amber Caution) (GV) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations (for Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

285 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS CONT PNL FAIL (Amber Caution) (GV) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

286 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS Fail - Select Manual (Amber Caution) (GV-SP/GIV-X) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations (for Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

287 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS Fail - Select Manual (Amber Caution) (GV-SP/GIV-X) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

288 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS FAIL-SEL MAN (Amber Caution) (GV) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM Limitations (for Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi), and f) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

289 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS FAIL-SEL MAN (Amber Caution) (GV) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched in unpressurized configuration provided: a) Manual pressurization is selected, b) The outflow valve is slewed to the full open position, c) Both engine bleeds and air conditioning packs are selected ON if available, or RAM Air is selected ON, d) Cabin pressure is monitored to be nominally zero psid during the flight, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will ensure required items e.g. Manual Pressurization Control System, Cabin Altitude and Cabin Rate of Climb Indicator and Auto Pilot are functional. Flight crew will operate the airplane in accordance with AFM Limitations. For Taxi, Takeoffs and Landings Max Cabin Pressure Differential 0.3 psi. To operate the airplane unpressurized, select manual pressurization and slew outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor cabin differential pressure to be nominally zero psid during the flight.

290 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS LAND ELEV FL (Blue Advisory) (GV) CPCS Landing Elevation Fail (Blue Advisory) (GV-SP/GIV-X) CPCS Maintenance Required (Blue Advisory) (GV-SP/GIV-X) CPCS MAINT REQD (Blue Advisory) (GV) CPCS Select Panel Fault (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched provided pressurization system is operated in the Semi mode. B Aeroplane may be dispatched provided pressurization system is operated in the Semi mode. C Aeroplane may be dispatched. C Aeroplane may be dispatched. A Aeroplane may be dispatched provided: a) Auto system (Cabin Pressure Control Panel) is operative, b) Semi-auto mode is considered inoperative, and c) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures

291 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message CPCS SEL PNL FAULT (Blue Advisory) (GV) CVR FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Aeroplane may be dispatched provided: a) Auto system (Cabin Pressure Control Panel) is operative, b) Semi-auto mode is considered inoperative, and c) Repairs are made within two (2) flight days. A One or more may be inoperative provided: a) Not more than 72 hours have elapsed since cockpit voice recorder was found to be unserviceable, b) Aeroplane does not exceed 8 further consecutive flights with cockpit voice recorder unserviceable, and c) Any flight data recorder required to be carried is operative. PAGE NO: Operational Procedures

292 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Database Config (Blue Advisory) (GV-SP/GIV-X) DAU 1A FL DAU 1B FL DAU 2A FL DAU 2B FL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Except where en route operations or minimums require a current database, aeroplane may be dispatched with charts out of currency provided: a) Current Aeronautical Charts are used to verify Navigation fixes before dispatch, b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and c) Approach Navigation Radios are manually tuned and identified. A (O) Aeroplane may be dispatched with one (1) failed DAU channel provided: a) Flight crew selects operative channel via the display controller, and b) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will select operative channel via the display controller.

293 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message DISP CTRL 2 FAIL (Blue Advisory) (GV) 1. MMEL REV. NO: 1 MMEL DATE: 2. MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aircraft may be dispatched provided: a) The weather at the destination is forecast to be VFR, b) An alternate airport is specified in the flight plan which has VFR weather forecast, c) Both VOR and ADF navigation receivers are operative, d) Flight is conducted based on short range navigation sources only being available, e) Navigation suffix in the IFR flight plan clearly indicates that the aeroplane is not capable of any RNP required navigation capability, f) Flight is conducted in airspace where the availability of navigation by short range navigation receivers (VOR/ADF) is assured, g) One DBDI or Standby RMI or Secondary Navigation Display is operative, h) Alternate procedures are established and used, i) Flight crew pull and collar DISP CONT #2: REER, C-2 Display Controller circuit breaker. Flight crew may accomplish this task if properly qualified and authorized, j) Flight crew prepare and display a TOLD (Takeoff and Landing Data) card prior to takeoff and prior to approach and landing (GV only), k) Flight crew verify required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable, l) Pilot-Not-Flying (PNF) is prepared to announce approach minimums in the event the operative Display Controller fails en route, and m) Repairs are made within one (1) flight day. PAGE NO: Operational Procedures Flight crew will ensure the DISP CONT #2: REER, C-2 circuit breaker for the failed Display Controller is pulled and collared. The flight crew shall prepare and display a TOLD (Takeoff and Landing Data) card prior to takeoff and prior to approach and landing.

294 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Display Controller 2 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aircraft may be dispatched provided: a) FMS is the navigation source on both PFD s, b) Destination and alternate airports have either LPV, GPS or FMS overlay approaches available without NOTAM restrictions for aeroplanes not equipped with Enhanced Navigation Package, c) Destination and alternate airports have either LPV, GPS, FMS overlay, or ILS approach available without NOTAM restrictions for aeroplanes equipped with Enhanced Navigation Package, d) No other display system failures exist, e) Flight crew pull and collar DISP CONT #2: REER, C-2 Display Controller circuit breaker. Flight crew may accomplish this task if properly qualified and authorized, f) Alternate procedures are established and used, g) Pilot-Not-Flying (PNF) is prepared to announce approach minimums in the event the operative Display Controller fails en route, and h) Repairs are made within one (1) flight day. PAGE NO: Operational Procedures Flight crew will pull and collar the DISP CONT #2 REER C-2 Display Controller circuit breaker. Flight crew will verify the required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable. When weather conditions exist at the destination or alternate airport during the approach, the PNF will be prepared to announce approach minimums in the event the operative Display Controller fails en route.

295 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message DME 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) EGPWM SYS 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) Elevator Trim 1-2 Fail (Amber Caution) (GV-SP/GIV-X) ELEV TRIM INOP (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C Aeroplane may be dispatched except where en route operations or approach minimums require its use. B Aeroplane may be dispatched. NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction. B (O) Aeroplane may be dispatched with electric elevator trim inoperative provided: a) Electric Elevator Trim remains OFF, b) Both Flap/Stabilizer Control Channels are operative (no messages on CAS), and c) Aeroplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed 0.80 Mach). B (O) Aeroplane may be dispatched with electric elevator trim inoperative provided: a) Electric Elevator Trim remains OFF, b) Both Flap/Stabilizer Control Channels are operative (no messages on CAS), and c) Aeroplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed 0.80 Mach). PAGE NO: Operational Procedures Flight crew will ensure electronic Pitch Trim remains OFF, both Flap/Stabilizer Control Channels are operative (no messages on CAS), and airplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed is 0.80 Mach). Flight crew will ensure electronic Pitch Trim remains OFF, both Flap/Stabilizer Control Channels are operative (no messages on CAS), and airplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed is 0.80 Mach).

296 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Engine Maintenance ###, L-R (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with Blue Engine Maintenance STD (###) and/or Engine Maintenance LTD messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: Blue Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue Engine Maintenance LTD messages required maintenance action within 500 hours. PAGE NO: Operational Procedures GV-SP: Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff. GIV-X: Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff.

297 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Engine Maintenance LTD, L-R (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with Blue Engine Maintenance STD (###) and/or Engine Maintenance LTD messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: Blue Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue Engine Maintenance LTD messages required maintenance action within 500 hours. PAGE NO: Operational Procedures GV-SP: (O) Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff. GIV-X: Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff.

298 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ENG MAINT ###, L-R (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with Blue Engine Maintenance STD (###) and/or Engine Maintenance LTD messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: Blue Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue Engine Maintenance LTD messages required maintenance action within 500 hours. PAGE NO: Operational Procedures Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff.

299 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ENG MAINT LTD, L-R (Blue Advisory) (GV) EPS Maintenance Reqd, L-R (Blue Advisory) (GV-SP/GIV-X) EPS MAINT REQD, L-R (Blue Advisory) (GV) EVS Fail (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with Blue Engine Maintenance STD (###) and/or Engine Maintenance LTD messages displayed on EICAS provided: a) Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and b) FADEC faults are reviewed by flight crew before each takeoff. NOTE: Blue Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue Engine Maintenance LTD messages required maintenance action within 500 hours. C Aeroplane may be dispatched. C Aeroplane may be dispatched. C Aeroplane may be dispatched and EVS shall not be used. PAGE NO: Operational Procedures Flight crew will ensure repairs are made in accordance with times (hours) established. Flight crew will review FADEC faults prior to each takeoff.

300 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message EVS FAIL (Amber Caution) (GV) EVS Maintenance Required (Blue Advisory) (GV-SP/GIV-X) EVS MAINT REQD (Blue Advisory) (GV) EVS Window Heat Fail (Amber Caution) (GV-SP/GIV-X) EVS WINDOW HEAT FAIL (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C Aeroplane may be dispatched and EVS shall not be used. C If EVS display is not normal, aeroplane may be dispatched provided EVS is not used. C If EVS display is not normal, aeroplane may be dispatched provided EVS is not used. C If EVS display is not normal, aeroplane may be dispatched provided EVS is not used. C If EVS display is not normal, aeroplane may be dispatched provided EVS is not used. PAGE NO: Operational Procedures

301 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FDAU FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A One or more may be inoperative provided: a) Aeroplane does not exceed 8 further consecutive flights with flight data recorder unserviceable, b) Not more than 72 hours have elapsed since flight data recorder was found to be unserviceable, and c) Any cockpit voice recorder required to be carried is operative. NOTE 1: Flight data recorder is considered to be inoperative when any of the following conditions exist: a) Loss of flight recording function is evident to flight crew during pre-flight check e.g. by means of a system status monitor, b) Need for maintenance has been identified by system monitors, where available, with setting of an indicator and cause of that setting has not been determined, or c) Analysis of recorded data or maintenance actions have shown that more than 5% of the total number of individual parameters (variable and discrete), required to be recorded for the particular aircraft, are not being recorded properly. NOTE 2: Where improper recording affects 5% of the parameters or less, timely corrective action will need to be taken by aeroplane operator in accordance with approved maintenance procedures. PAGE NO: Operational Procedures

302 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FDR SYS FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A One or more may be inoperative provided: a) Aeroplane does not exceed 8 further consecutive flights with flight data recorder unserviceable, b) Not more than 72 hours have elapsed since flight data recorder was found to be unserviceable, and c) Any cockpit voice recorder required to be carried is operative. NOTE 1: Flight data recorder is considered to be inoperative when any of the following conditions exist: a) Loss of flight recording function is evident to flight crew during pre-flight check e.g. by means of a system status monitor, b) Need for maintenance has been identified by system monitors, where available, with setting of an indicator and cause of that setting has not been determined, or c) Analysis of recorded data or maintenance actions have shown that more than 5% of the total number of individual parameters (variable and discrete), required to be recorded for the particular aircraft, are not being recorded properly. NOTE 2: Where improper recording affects 5% of the parameters or less, timely corrective action will need to be taken by aeroplane operator in accordance with approved maintenance procedures. PAGE NO: Operational Procedures

303 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FDR System Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A One or more may be inoperative provided: a) Aeroplane does not exceed 8 further consecutive flights with flight data recorder unserviceable, b) Not more than 72 hours have elapsed since flight data recorder was found to be unserviceable, and c) Any cockpit voice recorder required to be carried is operative. NOTE 1: Flight data recorder is considered to be inoperative when any of the following conditions exist: a) Loss of flight recording function is evident to flight crew during pre-flight check e.g. by means of a system status monitor, b) Need for maintenance has been identified by system monitors, where available, with setting of an indicator and cause of that setting has not been determined, or c) Analysis of recorded data or maintenance actions have shown that more than 5% of the total number of individual parameters (variable and discrete), required to be recorded for the particular aircraft, are not being recorded properly. NOTE 2: Where improper recording affects 5% of the parameters or less, timely corrective action will need to be taken by aeroplane operator in accordance with approved maintenance procedures. PAGE NO: Operational Procedures

304 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FGC 1-2 FAIL (Amber Caution) (GV) Fire Detection Loop Fault (Amber Caution) (GV-SP/GIV-X) FIRE DET LOOP FALT (Amber Caution) (GV) Flap/Stab Maint Reqd A-B (Blue Advisory) (GV-SP) Flap/Stab Maint Reqd (Blue Advisory) (GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations or where en route operations or approach minimums require its use, aeroplane may be dispatched with one (1) failed provided aeroplane is operated in accordance with AFM Limitations in the event the operative FGC fails and the Yaw Damper is inoperative. NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations. B Except for ER operations, aeroplane may be dispatched with one (1) complete loop (A or B) inoperative provided the Fault Switch/Light is pressed to isolate the faulty loop and illuminate the OFF portion of the switch light. B Except for ER operations, aeroplane may be dispatched with one (1) complete loop (A or B) inoperative provided the Fault Switch/Light is pressed to isolate the faulty loop and illuminate the OFF portion of the switch light. C Aeroplane may be dispatched. C Aeroplane may be dispatched. PAGE NO: Operational Procedures Flight crew will observe AFM limitations in the event the operative FGC fails and the Yaw Damper is inoperative.

305 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Flap/Stab System Fail A-B (Blue Advisory) (GV-SP) FLP/STB MX RQD A-B (Blue Advisory) (GV) FLP/STB SYS FL A-B (Blue Advisory) (GV) FMS/GPS Pos Monitor Unavail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Aeroplane may be dispatched with one (1) channel inoperative provided: a) Electric Pitch Trim System is operative, b) Alternate control is verified to be operative before each departure, and c) Repairs are made within two (2) flight days. C Aeroplane may be dispatched. A Aeroplane may be dispatched with one (1) channel inoperative provided: a) Electric Pitch Trim System is operative, d) Alternate control is verified to be operative before each departure, and e) Repairs are made within two (2) flight days. B (O) Aeroplane may be dispatched provided: a) FMS position is checked against available sensors, and b) If errors encountered, affected GPS is deselected as a position sensor and FMS position is updated. PAGE NO: Operational Procedures Check FMS position against available sensors. De-select GPS as a position sensor and update FMS position if errors encountered.

306 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FMS Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Aeroplane may be dispatched with two (2) inoperative except where en route operations or approach minimums require its use provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMU s are operative (GV), and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. RNP RNAV including PRNAV and BRNAV only require a single FMS. PAGE NO: Operational Procedures

307 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FMS 1-2 FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Aeroplane may be dispatched with two (2) inoperative except where en route operations or approach minimums require its use provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMU s are operative (GV), and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. RNP RNAV including PRNAV and BRNAV only require a single FMS. PAGE NO: Operational Procedures

308 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Forward Cabin Temp Fan Fail (Blue Advisory) (GV-SP/GIV-X) FQMS Maintenance Required (Blue Advisory) (GV-SP/GIV-X) FQMS MAINT REQD (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail; b) Forward Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) FWD CABIN SENSOR FAN, LEER D-9, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and e) Flight crew monitor forward cabin temperature and forward cabin duct temperature. C Aeroplane may be dispatched. C Aeroplane may be dispatched. PAGE NO: Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail, b) Forward Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) FWD CABIN SENSOR FAN circuit breaker: LEER D-9 is pulled and collared, and e) Forward cabin temperature and Forward cabin duct temperature are monitored.

309 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FQSC Channel Fail, L-R (Blue Advisory) (GV-SP/GIV-X) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with one (1) channel inoperative provided: a) Both tanks are completely filled using overwing refueling in accordance with the Aircraft Operating Manual, Section , b) Both Fuel Flow Indicating Systems are operative, c) After takeoff, power is set by matching fuel flow indications on both engines, and d) Flight crew maintains a log of fuel burned. NOTE: Total Fuel indications will be INVALID with inoperative indicator. PAGE NO: Operational Procedures Flight crew will ensure BOTH tanks are completely filled using overwing method of fueling. NOTE: Do not pull Fuel Qty circuit breaker as this disables Fuel Level Low caution message. Flight crew will ensure: a) Both Fuel Flow Indicating Systems are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator.

310 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FQSC Channel Fail, L-R (Blue Advisory) (GV-SP/GIV-X) (cont d) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with one (1) channel inoperative provided: a) Affected tank is defueled before each refueling in accordance with the Aircraft Operating Manual, Section , b) Affected tank is fueled with a known quantity of fuel, c) Both fuel flow meters are operative, d) After takeoff, power is set by matching fuel flow indications on both engines, and e) Flight crew maintains a log of fuel burned. NOTE: Total Fuel indications will be INVALID with inoperative indicator. PAGE NO: Operational Procedures Flight crew will Defuel affected tank before each refueling and refuel it with a Known quantity of fuel. Flight crew will ensure: a) Both fuel flow meters are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator.

311 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FQSC CH FAIL, L-R (Blue Advisory) (GV) (continued) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with one (1) channel inoperative provided: a) Both tanks are completely filled using overwing refueling in accordance with the Aircraft Operating Manual, Section , b) Both Fuel Flow Indicating Systems are operative, c) After takeoff, power is set by matching fuel flow indications on both engines, and d) Flight crew maintains a log of fuel burned. NOTE: Total Fuel indications will be INVALID with inoperative indicator. PAGE NO: Operational Procedures Flight crew will ensure BOTH tanks are completely filled using overwing method of fueling. NOTE: Do not pull Fuel Qty circuit breaker as this disables Fuel Level Low caution message. Flight crew will ensure: a) Both Fuel Flow Indicating Systems are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator

312 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FQSC CH FAIL, L-R (Blue Advisory) (GV) (cont d) Front Windshield Fail, L-R (Amber Caution) (GV-SP/GIV-X) Front Windshield Fault, L-R (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with one (1) channel inoperative provided: a) Affected tank is defueled before each refueling in accordance with the Aircraft Operating Manual, Section , b) Affected tank is fueled with a known quantity of fuel, c) Both fuel flow meters are operative, d) After takeoff, power is set by matching fuel flow indications on both engines, and e) Flight crew maintains a log of fuel burned. NOTE: Total Fuel indications will be INVALID with inoperative indicator. B Except for ER operations, one may be inoperative provided: a) Aeroplane is not operated in known or forecast icing conditions, and b) Both side window heat systems are operative. C Aeroplane may be dispatched with one inoperative sensor in each Windshield Heat System. PAGE NO: Operational Procedures Flight crew will Defuel affected tank before each refueling and refuel it with a Known quantity of fuel. Flight crew will ensure: a) Both fuel flow meters are operative. b) After takeoff, power is set by matching Fuel Flow indications on both engines. c) A log of fuel burned is maintained. NOTE: Total Fuel indication will be INVALID with inoperative indicator.

313 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Fuel Crossflow Valve Open (Amber Caution) (GV-SP/GIV-X) Fuel Return Fail, L-R (Blue Advisory) (GV-SP) FUEL RETURN FL, L-R (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with inoperative crossflow valve provided: a) All Fuel Boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative, d) Fuel Tank Temperature System is operative, and e) Aeroplane is operated in accordance with AFM Limitations. NOTE: Avoid uncoordinated maneuvers when Fuel Intertank Valve is OPEN. B Aeroplane may be dispatched provided: a) Flight crew monitors fuel tank temperature, and b) Aeroplane is operated in accordance with AFM Limitations. B Aeroplane may be dispatched provided: a) Flight crew monitors fuel tank temperature, and b) Aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures Flight crew will ensure: a) All Fuel boost Pumps are operative, b) Fuel Intertank Valve is operative, c) Fuel Quantity Indicating System is operative, d) Fuel tank temperature system is operative.

314 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message FWD CAB TMP FAN FL (Blue Advisory) (GV) F WSHLD FAIL, L-R (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail; b) Forward Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) FWD CABIN SENSOR FAN, LEER D-9, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and e) Flight crew monitor forward cabin temperature and forward cabin duct temperature. B Except for ER operations, one may be inoperative provided: a) Aeroplane is not operated in known or forecast icing conditions, and b) Both side window heat systems are operative. PAGE NO: Operational Procedures Flight crew will ensure: a) None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail, b) Forward Cabin Temperature Manual mode is operative, c) Associated temperature indicator is operative, d) FWD CABIN SENSOR FAN circuit breaker: LEER D-9 is pulled and collared, and e) Forward cabin temperature and Forward cabin duct temperature are monitored.

315 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message GCU Fail, L-R (Blue Advisory) (GV-SP/GIV-X) GCU FAIL, L-R (Blue Advisory) (GV) Generator Fail, L-R (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Except for ER Operations, aeroplane may be dispatched with one Engine Generator Control Unit (GCU) inoperative provided: a) APU Generator is used for all phases of flight, b) Aeroplane is operated at or below FL450, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. A Except for ER Operations, aeroplane may be dispatched with one Engine Generator Control Unit (GCU) inoperative provided: a) APU Generator is used for all phases of flight, b) Aeroplane is operated at or below FL450, c) Standby Electrical System is operative, and d) Repairs are made within two (2) flight days. A Except for ER Operations, aeroplane may be dispatched with one Engine Generator inoperative provided: a) Opposite Generator and GCU is operative, b) APU Generator is used for all phases of flight, c) Aeroplane is operated at or below FL450, d) Standby Electrical System is operative, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures

316 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message GEN FAIL, L-R (Blue Advisory) (GV) GPS 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) GPS 1-2 FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Except for ER Operations, aeroplane may be dispatched with one Engine Generator inoperative provided: a) Opposite Generator and GCU is operative, b) APU Generator is used for all phases of flight, c) Aeroplane is operated at or below FL450, d) Standby Electrical System is operative, and e) Repairs are made within two (2) flight days. B Aeroplane may be dispatched except where en route operations or approach minimums require the use of GPS or GNSSU. B Aeroplane may be dispatched except where en route operations or approach minimums require the use of GPS or GNSSU. PAGE NO: Operational Procedures

317 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message GPWS 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) GPWS FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched provided: a) Alternate procedures are established and used, b) Pilot-Not-Flying (PNF) monitors flight progress with reference to radio altimeter data and situational awareness, c) PNF advises Pilot-Flying (PF) of adverse situations, d) Aeroplane is operated in accordance with AFM Limitations, and e) Repairs or replacements are carried out within 6 further flights or 25 flying hours or 2 calendar days, whichever occurs first. A (O) Aeroplane may be dispatched provided: a) Alternate procedures are established and used, b) Pilot-Not-Flying (PNF) monitors flight progress with reference to radio altimeter data and situational awareness, c) PNF advises Pilot-Flying (PF) of adverse situations, d) Aeroplane is operated in accordance with AFM Limitations, and e) Repairs or replacements are carried out within 6 further flights or 25 flying hours or 2 calendar days, whichever occurs first. PAGE NO: Operational Procedures Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations Pilot-Not-Flying (PNF) will monitor flight progress with reference to radio altimeter data and situational awareness and advise Pilot-Flying (PF) of adverse situations

318 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message HUD COMP Fan Fail (Blue Advisory) (GV-SP/GIV-X) HUD OHU Fan Fail (Blue Advisory) (GV-SP/GIV-X) Hydraulic Temp Sen Fail, L-R (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C Aeroplane may be dispatched provided extended ground operations are avoided. C Aeroplane may be dispatched, provided: a) Extended ground operations are avoided, and b) Pilot selected HUD brightness is reduced. A Aeroplane may be dispatched provided repairs are made within two (2) flight days. NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures. PAGE NO: Operational Procedures

319 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message HYD TMP SEN FL, L-R (Blue Advisory) (GV) Ice Detect Fail, L-R (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Aeroplane may be dispatched provided repairs are made within two (2) flight days. NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures. B (O) Aeroplane may be dispatched provided: a) Aeroplane is operated in accordance with alternate AFM procedures, b) Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and SAT is +10 deg C or less, and c) Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges. NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available. PAGE NO: Operational Procedures Operate airplane in accordance with Alternate AFM procedures. Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and the SAT is +10 deg C or less. Wing Anti- Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges

320 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message ICE DETECT FL, L-R (Amber Caution) (GV) IRS Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched provided: a) Aeroplane is operated in accordance with alternate AFM procedures, b) Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and SAT is +10 deg C or less, and c) Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges. NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available. A (O) Aeroplane may be dispatched with one (1) IRS inoperative provided: a) Both PFD attitude indicating systems operate independently, b) Flight crew ensure same IRS is NOT used as attitude source for both pilots, c) Standby Attitude Indicator is operative, and d) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Operate airplane in accordance with Alternate AFM procedures. Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and the SAT is +10 deg C or less. Wing Anti- Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges Flight crew will ensure the same IRS is NOT used as attitude source for both pilots.

321 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message IRS FAIL (Blue Advisory) (GV) IRS ON DC (Blue Advisory) (GV) IRU On Sec Pwr (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with one (1) IRS inoperative provided: a) Both PFD attitude indicating systems operate independently, b) Flight crew ensure same IRS is NOT used as attitude source for both pilots, c) Standby Attitude Indicator is operative, and d) Repairs are made within two (2) flight days. A Aeroplane may be dispatched provided only one (1) IRU / IRS is on Secondary Power provided repairs are made within one (1) flight day. A Aeroplane may be dispatched provided only one (1) IRU / IRS is on Secondary Power provided repairs are made within one (1) flight day. PAGE NO: Operational Procedures Flight crew will ensure the same IRS is NOT used as attitude source for both pilots.

322 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message IRU Sec Pwr Fail (Blue Advisory) (GV-SP/GIV-X) LASERTRAK FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Aeroplane may be dispatched with one back-up battery inoperative provided: a) The affected battery is located in the #2 or #3 IRU back up battery position, and b) Repairs are made within one (1) flight day. A Aeroplane may be dispatched with two (2) backup batteries inoperative provided: a) Aeroplane is operated in day VMC conditions, and b) Repairs are made within one (1) flight day. A Aeroplane may be dispatched with two (2) backup batteries inoperative provided: a) All other components of the Electrical Power system are operative, and b) Repairs are made within one (1) flight day. B Aeroplane may be dispatched provided at least one Flight Management System is operative. PAGE NO: Operational Procedures

323 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message L PSU Fan Fail (Blue Advisory) (GV-SP/GIV-X) LX Fail (Blue Advisory) (GV-SP/GIV-X) Mach Trim 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched provided: a) Ambient Temperature is 95 degrees F (35 degrees C) or cooler, b) TRU electrical loads are 50% or less, c) Right main TRU is operative, d) Both Environmental Control System (ECS) Packs are operative, e) Flight crew minimize ground operation time, and f) For ground operations longer than 15 minutes, flight crew ensure main and baggage doors are closed, APU air is selected ON and outflow valve is fully OPEN. C Aeroplane may be dispatched. B Aeroplane may be dispatched with one (1) Mach Trim System inoperative. PAGE NO: Operational Procedures Flight crew will: a) Minimize ground operation time, espescially during hot weather. b) During Ground operation, monitor TRU load limit load to 50%. For ground operation longer than 15 minutes ensure main and baggage doors are closed. APU air is selected ON and outflow valve is fully OPEN.

324 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message MADC FAIL (Blue Advisory) (GV) 1. MMEL REV. NO: 1 MMEL DATE: 2. MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched with a one (1) micro air data computer inoperative provided: a) Manual Pressurization Control System is operative, b) Cabin Altitude and Differential Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is operative, d) Autopilot is operative, e) Aeroplane is operated in accordance with AFM limitations, f) MADC 1: POP A-9, MADC 2: CPOP A-9, and MADC 3: POP A-10 circuit breakers associated with the failed Micro Air Data Computer (MADC) are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and g) Flight crew selects operative and different MADC sources prior to departure. NOTE 1: Two systems are required for operation in RVSM airspace. NOTE 2: For MADC 1 FAIL, expect the L Engine Backup Air Data advisory and associated Engine Maintenance message to post. NOTE 3: For MADC 2 FAIL, expect the R Engine Backup Air Data advisory and associated Engine Maintenance message to post. B (O) Aeroplane may be dispatched with one (1) micro air data computer inoperative provided aeroplane is operated in unpressurized configuration. PAGE NO: Operational Procedures Flight crew will pull and collar MADC 1: POP A-9, MADC 2: CPOP A-9, and MADC 3: POP A-10 circuit breaker associated with Micro Air Data Computers. Flight crew will operationally check and assure that the items called out in provisos a) thru d) are operative. Flight crew will comply with all AFM limitations in section , , and To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to full open position with both engine bleeds and air conditioning packs selected ON if available. If not, select RAM Air ON. Monitor Cabin differential pressure to be nominally zero psid during the flight.

325 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message MADC 1-3 PROBE FL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched with one (1) probe heater inoperative provided: a) Aeroplane is not operated in visible moisture or known or forecast icing conditions, b) L LWR PITOT HTR: POP A-5 and R LWR PITOT HTR: CPOP A-5 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, c) Flight crew select MADC sources that are different and not associated with failed pitot heater element, d) Dispatch is not authorized in conjunction with MADC 2-SBY PROBE FL, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar L LWR PITOT HTR: POP A-5 and R LWR PITOT HTR: CPOP A-5 circuit breakers and select MADC sources that are different and not associated with failed pitot heater element.

326 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message MADC 2-SBY PROBE FL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Except for ER operations, aeroplane may be dispatched with one (1) probe heater inoperative provided: a) Aeroplane is not operated in visible moisture or known or forecast icing conditions, b) L UPR PITOT HTR: POP A-6 and R UPR PITOT HTR: CPOP A-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, c) Flight crew select MADC sources that are different and not associated with failed pitot heater element, and d) Dispatch is not authorized in conjunction with MADC 1-2 PROBE FL, and e) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar L UPR PITOT HTR: POP A-6 and R UPR PITOT HTR: CPOP A-4 circuit breakers and select MADC sources that are different and not associated with failed pitot heater element.

327 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Main Fuel Pump Fail, L-R (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with one (1) pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, e) Dispatch is not authorized in conjunction with Alternate Pump Fail, L-R or with Alt FuelPump Fail, L-R, and f) Aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure.

328 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message MAIN PUMP FAIL, L-R (Amber Caution) (GV) MAINT REQUIRED (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with one (1) pump inoperative provided: a) Fuel Crossflow Valve is operative, b) Fuel Intertank Valve is operative, c) Both Fuel Low Quantity Warning Systems are operative, d) Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, e) Dispatch is not authorized in conjunction with ALT PUMP FAIL, L-R, and f) Aeroplane is operated in accordance with AFM Limitations. C Aeroplane may be dispatched. PAGE NO: Operational Procedures Flight crew will ensure: a) Fuel Crossflow Valve and Intertank Valve are operative, b) BOTH Fuel Low Quantity Warning Systems are operative, c) Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure.

329 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Main TRU Fault, L-R (Amber Caution) (GV-SP/GIV-X) MAU Fan Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with one (1) main TRU inoperative provided: a) Both Generators are operative, b) Both essential TRU s are operative, c) Auxiliary TRU is operative, d) APU Generator is operative, e) Both Battery chargers are operative, f) Both Main Aeroplane Batteries are operative, g) Inoperative L MAIN TRU: LPDB, Left Main AC section or R MAIN TRU: RPDB, Right Main AC section TRU circuit breaker on the Power Distribution Box is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and h) Repairs are made within two (2) flight days. A Aeroplane may be dispatched: a) With one (1) failed fan provided performance of items affected by the indicated MAU are monitored during the flight, b) Flight crew references the appropriate matrix in AFM Section , and c) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar inoperative L MAIN TRU: LPDB, Left Main AC section or R MAIN TRU: RPDB, Right Main AC section TRU circuit breaker on Power Distribution Box. Flight crew will ensure AUX TRU is operative and both essential TRUs are operative.

330 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message MAU 1B-2A-3A-3B Fail (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with one (1) channel inoperative provided: a) Failed channel is not MAU 1A or MAU 2B, and b) No other failures exist in the Avionics System, c) MAU circuit breakers associated with the failed MAU channel are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized: MAU 1A PRI: POP, A-10 MAU 1A SEC: CPOP, A-10 MAU 1B PRI: CPOP, A-9 MAU 1B SEC: POP, A-9 MAU 2A PRI: CPOP, A-8 MAU 2A SEC: POP, A-8 MAU 2B PRI: CPOP, A-7 MAU 2B SEC: POP, A-7 MAU 3A PRI: POP, A-6 MAU 3A SEC: CPOP, A-6 MAU 3B PRI: POP, A-5 MAU 3B SEC: CPOP, A-5, d) Alternate procedures are established and used, e) Flight crew discusses contingency procedures for next worse failures as described in GAC- OIS-09 Dispatch with MAU Channels Inoperative, and f) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar the associated MAU circuit breakers: MAU 1A PRI: POP, A-10 MAU 1A SEC: CPOP, A-10 MAU 1B PRI: CPOP, A-9 MAU 1B SEC: POP, A-9 MAU 2A PRI: CPOP, A-8 MAU 2A SEC: POP, A-8 MAU 3A PRI: POP, A-6 MAU 3A SEC: CPOP, A-6 MAU 3B PRI: POP, A-5 MAU 3B SEC: CPOP, A-5 Flight crew will review the next worse failures as described in the GAC-OIS-09 Dispatch with MAU Channels Inoperative. Flight crew will discuss contingency procedures should the next worse failure occur and plan accordingly for the flight.

331 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message MDAU FAIL (Blue Advisory) (GV) MDAU MEM 90% FULL (Blue Advisory) (GV) MN TRU FAULT, L-R (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched provided all faults are recorded after each flight. B Aeroplane may be dispatched provided all faults are recorded after each flight. A (O) Aeroplane may be dispatched with one (1) main TRU inoperative provided: a) Both Generators are operative, b) Both essential TRU s are operative, c) Auxiliary TRU is operative, d) APU Generator is operative, e) Both Battery chargers are operative, f) Both Main Aeroplane Batteries are operative, g) Inoperative L MAIN TRU: LPDB, Left Main AC section or R MAIN TRU: RPDB, Right Main AC section TRU circuit breaker on the Power Distribution Box is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and h) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar inoperative L MAIN TRU: LPDB, Left Main AC section or R MAIN TRU: RPDB, Right Main AC section circuit breaker on Power Distribution Box. Flight crew will ensure AUX TRU is operative and both essential TRUs are operative.

332 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message MRC 1 Fail (Amber Caution) (GV-SP/GIV-X) MRC 2 Fail (Blue Advisory) (GV-SP/GIV-X) NAV 2 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Aeroplane may be dispatched with one (1) MRC failed, provided: a) Associated Comm and Nav radios and opposite ATC are operative, b) Dispatch should not be authorized in conjunction with MRC 2 fail, and c) Repairs are made within one (1) flight day. NOTE: EICAS blue messages APM FAIL and ASCB FAIL displayed. ASCB FAIL is only displayed in flight. A Aeroplane may be dispatched provided: a) Associated Comm and Nav radios and opposite ATC are operative, b) Dispatch should not be authorized in conjunction with MRC 1 Fail, and c) Repairs are made within one (1) flight day. NOTE: With MRC 2 Fail, expect EICAS blue messages APM FAIL and ASCB FAIL displayed. ASCB FAIL will display inflight only. B Aeroplane may be dispatched as required by Operating Requirements. PAGE NO: Operational Procedures

333 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message NAVCOM Fail (Blue Advisory) (GV-SP/GIV-X) NMS 1-2 FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched provided operations do not require its use. A Except where en route operations or approach minimums require its use, aeroplane may be dispatched provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMUs are operative, and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. PAGE NO: Operational Procedures

334 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message NMS FAIL (Blue Advisory) (GV) NWS Fixed Gain (Blue Advisory) (GV-SP/GIV-X) NWS FIXED GAIN (Blue Advisory) (GV) Outflow Valve Fault (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Except where en route operations or approach minimums require its use, aeroplane may be dispatched provided: a) Affected system is not required for IRS alignment, b) Long Range Navigation is not dependent on its use, c) Procedures do not require its use, d) Both RFMUs are operative, and e) Repairs are made within two (2) flight days. NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace. B Aeroplane may be dispatched provided Nose Wheel Tiller Steering System is operative. B Aeroplane may be dispatched provided Nose Wheel Tiller Steering System is operative. B Aeroplane may be dispatched provided: a) DC motor is operative, and b) Aeroplane is operated in accordance with AFM Limitations. PAGE NO: Operational Procedures

335 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message OUTFLOW VLV FAULT (Blue Advisory) (GV) Pitch Trim 1-2 Power Fail (Blue Advisory) (GV-SP/GIV-X) RAAS 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) RAD ALT 1-2 FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched provided: a) DC motor is operative, and b) Aeroplane is operated in accordance with AFM Limitations. B (O) Aeroplane may be dispatched with one (1) inoperative Autopilot Pitch Trim Servo provided PITCH TRIM SERVO #1: POP, E-2 or PITCH TRIM SERVO #2, CPOP, E-1 circuit breaker is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. B Aeroplane may be dispatched. B Aeroplane may be dispatched provided: a) Landing weather minimums or operating procedures do not require its use, and b) Other systems affected (E/GPWS, TCAS, Flight Director, Autopilot, Autothrottle, Altimeter Ground Awareness Display, Synthetic Vision Primary Flight Display, HUD Flare Cue) are considered. PAGE NO: Operational Procedures Flight crew will ensure inoperative PITCH TRIM SERVO #1: POP, E-2 or PITCH TRIM SERVO #2, CPOP, E-1 servo circuit breaker is pulled and collared.

336 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Radio Altimeter 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) Rudder Steering Fail (Amber Caution) (GV-SP/GIV-X) RUDDER STRG FAIL (Amber Caution) (GV) SATCOM Call (Blue Advisory) (GIV-X/GV-SP) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched provided: a) Landing weather minimums or operating procedures do not require its use, and b) Other systems affected (E/GPWS, TCAS, Flight Director, Autopilot, Autothrottle, Altimeter Ground Awareness Display, Synthetic Vision Primary Flight Display, HUD Flare Cue) are considered. B Aeroplane may be dispatched provided: a) Nose Wheel Tiller Steering System is operative, and b) Left seat pilot performs the takeoff and landing task. B Aeroplane may be dispatched provided: a) Nose Wheel Tiller Steering System is operative, and b) Left seat pilot performs the takeoff and landing task. C Aeroplane may be dispatched provided procedures do not require their use. PAGE NO: Operational Procedures

337 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Service Door (Blue Advisory) (GV-SP/GIV-X) SERVICE DOOR (Blue Advisory) (GV) Side Windshield Fail, L-R (Amber Caution) (GV-SP/GIV-X) Single Rudder (Blue Advisory) (GV) Single Speed Brake (Blue Advisory) (GV-SP) SINGLE SPEED BRAKE (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Aeroplane may be dispatched provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED by: a) Door latches or lock handles are flush, and b) Door edges are flush with fuselage. B (O) Aeroplane may be dispatched provided a crewmember verifies by visual inspection before each departure that the associated door is CLOSED and LOCKED by: a) Door latches or lock handles are flush, and b) Door edges are flush with fuselage. B Aeroplane may be dispatched with one side windshield failed provided aeroplane is not operated into known or forecast icing conditions. B Aeroplane may be dispatched provided the Rudder Limitation indication is operative. B Aeroplane may be dispatched provided the Single Rudder indication is operative. B Aeroplane may be dispatched provided the Single Rudder indication is operative. PAGE NO: Operational Procedures Flight crew will visually inspect door(s) to ensure it is CLOSED and LOCKED prior to departure. Flight crew will visually inspect door(s) to ensure it is CLOSED and LOCKED prior to departure.

338 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message STCK PUSH 1-2 FAULT (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker circuit breakers associated with the failed system. Flight crew may accomplish this task if properly qualified and authorized: SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar the SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5 circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be crossreferenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case.

339 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message STCK PUSH 1-2 FL (Amber Caution) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker circuit breakers associated with the failed system. Flight crew may accomplish this task if properly qualified and authorized: SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar the SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5 circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be crossreferenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case.

340 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Stick Push 1-2 Fail (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker circuit breakers associated with the failed system. Flight crew may accomplish this task if properly qualified and authorized: SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar the SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5 circuit breakers for the Stall Barrier Valve and Stick Shaker associated with the failed system. Flight crew will discuss crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be crossreferenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case.

341 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Stick Push 1-2 Fault (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with one (1) system inoperative provided: a) Angle of Attack indication is available on both PFD s, b) Alternate procedures are established and used, c) The inoperative stall barrier system is electrically disabled by pulling and collaring the Stall Barrier Valve and Stick Shaker circuit breakers associated with the failed system. Flight crew may accomplish this task if properly qualified and authorized: SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5, d) Crew procedures in the event the remaining stall barrier fails are discussed, e) If the remaining stall barrier fails the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight (this minimum speed shall be cross referenced to a normalized AOA value of 0.59 as displayed on the PFD), f) Weather at departure and destination is considered, g) Consideration is given to delaying takeoff or approach and landing, if windshear is forecast until such conditions cease, or consideration is given to proceeding to alternate, and h) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures Flight crew will pull and collar the SHAKER #1: POP E-6, SHAKER #2: CPOP E-6, STALL BARR VALVE #1: POP E-5, STALL BARR VALVE #2: CPOP E-5 for the Stall Barrier Valve and Stick Shaker associated with the failed system. Prior to dispatch, the flight crew will discuss the dispatch situation with the stall barrier inoperative and crew procedures in the event the remaining operative stall barrier fails. If the remaining stall barrier fails, the minimum speed shall be no less than Vref (1.3 Vs) for all phases of flight. This minimum speed shall be cross-referenced to Normalized Angle of Attack of 0.59 as displayed on the PFD. Weather conditions at the departure and destination airports shall be considered. If there are known or forecast windshear conditions at the departure or destination airport, the crew shall consider delaying the takeoff or approach and landing until such conditions cease to exist, or consider deviation to an alternate airport in the approach and landing case.

342 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Stick Shake 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) STICK SHAKE 1-2 FL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A Aeroplane may be dispatched with a single control column shaker inoperative provided: a) Angle of Attack indication is available on both PFD s, b) Both stall barrier systems are operative, and c) Repairs are made within two (2) flight days. A Aeroplane may be dispatched with a single control column shaker inoperative provided: a) Angle of Attack indication is available on both PFD s, b) Both stall barrier systems are operative, and c) Repairs are made within two (2) flight days. PAGE NO: Operational Procedures

343 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Stuck MIC ACP 3 (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched with ACP 3 indicating stuck MIC provided: a) Pilot and Copilot ACP s are operative, b) OBSERVER ACP: REER, D-7, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, c) Affected ACP is not required as determined by the Pilot-in-Command, d) Flight Deck to cabin communication is operative, e) A passenger seat in the passenger cabin is made available to an inspector for the performance of official duties, f) Alternate procedures are established and used, g) Required minimum safety equipment (safety belt and oxygen) is available, h) Seat is acceptable to the inspector for performance of official duties, and i) Repairs are made within two (2) flight days. NOTE 1: These provisos are intended to provide for occupancy of the above seats by an inspector when the minimum safety equipment (oxygen and safety belt) is functional and the inspector determines the condition to be acceptable. NOTE 2: The pilot-in-command will determine if the minimum safety equipment is functional for other persons authorized to occupy any observer seat(s). PAGE NO: Operational Procedures Flight crew will ensure: a) Pilot and Copilot ACP s are operative, b) OBSERVER ACP: REER D-7, is pulled and collared, c) Affected ACP is not required as determined by the Pilotin-Command, d) Flight Deck to cabin communication is operative, and e) Alternate procedures are established and used.

344 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message S WSHLD FAIL, L-R (Amber Caution) (GV) TCAS Fail (Blue Advisory) (GV-SP/GIV-X) TCAS FAIL (Blue Advisory) (GV) Terrain 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched with one side windshield failed provided aeroplane is not operated into known or forecast icing conditions. A (O) Aeroplane may be dispatched provided: a) System is deactivated and secured by pulling and collaring TCAS: POP, F-2 circuit breaker. Flight crew may accomplish this task if properly qualified and authorized, b) En route or approach procedures do not require its use, and c) Repairs are made within two (2) flight days. A (O) Aeroplane may be dispatched provided: a) System is deactivated and secured by pulling and collaring TCAS: POP, F-2 circuit breaker. Flight crew may accomplish this task if properly qualified and authorized, b) En route or approach procedures do not require its use, and c) Repairs are made within two (2) flight days. B Aeroplane may be dispatched provided GPWS functions are operative. NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction. PAGE NO: Operational Procedures Flight crew will ensure: a) System is deactivated and secured by pulling and collaring TCAS Power POP, F-2 circuit breaker, and b) En route or approach procedures do not require its use. Flight crew will ensure: a) System is deactivated and secured by pulling and collaring TCAS Power POP, F-2 circuit breaker, and b) En route or approach procedures do not require its use.

345 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message Terrain Bus Fail (Blue Advisory) (GV-SP/GIV-X) THROT QUAD 1-2 FL (Blue Advisory) (GV) Throttle Quadrant 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) VHF COM 2 Fail (Blue Advisory) (GV-SP/GIV-X) VHF COMM 2 FAIL (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Aeroplane may be dispatched provided GPWS functions are operative. NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction. B Aeroplane may be dispatched. NOTE: With both Channel 1 and Channel 2 failed, the autothrottle system will be inoperative. B Aeroplane may be dispatched. NOTE: With both Channel 1 and Channel 2 failed, the autothrottle system will be inoperative. C Aeroplane may be dispatched with any in excess of those required by Operating Requirements. C Aeroplane may be dispatched with any in excess of those required by Operating Requirements. PAGE NO: Operational Procedures

346 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message WG A/I SYS FL, L-R (Amber Caution) (GV) Windshear 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B Except for ER operations, aeroplane may be dispatched with wing anti-ice system inoperative provided aeroplane is not operated in known or forecast icing conditions. NOTE: Do not select affected side Wing Anti-Ice to ON. A (O) Aeroplane may be dispatched provided: a) At least one (1) radio altimeter is operative, b) Alternate procedures are established and used, c) Flight crew comply with AFM/AOM guidance in windshear situations and recommended procedures when encountering windshear, and d) Repairs are made within two (2) flight days. NOTE: Operator s alternate procedures should include reviewing windshear avoidance and windshear recovery procedures. PAGE NO: Operational Procedures Flight crew will comply with AFM/AOM guidance in windshear situations and recommended procedures when encountering windshear and verify both radio altimeters are valid.

347 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message WINDSHEAR FAIL (Blue Advisory) (GV) Wing Anti-Ice Sys Fail, L-R (Amber Caution) (GV-SP/GIV-X) Yaw Damper 1-2 Fail (Amber Caution) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures A (O) Aeroplane may be dispatched provided: a) At least one (1) radio altimeter is operative, b) Alternate procedures are established and used, c) Flight crew comply with AFM/AOM guidance in windshear situations and recommended procedures when encountering windshear, and d) Repairs are made within two (2) flight days. NOTE: Operator s alternate procedures should include reviewing windshear avoidance and windshear recovery procedures. B Except for ER operations, aeroplane may be dispatched with wing anti-ice system inoperative provided aeroplane is not operated in known or forecast icing conditions. NOTE: Do not select affected side Wing Anti-Ice to ON. B (O) Except for ER operations, aeroplane may be dispatched with one (1) channel inoperative provided aeroplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. PAGE NO: Operational Procedures Flight crew will comply with AFM/AOM guidance in windshear situations and recommended procedures when encountering windshear and verify both radio altimeters are valid. Flight crew will ensure airplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails.

348 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message YD 1-2 FAIL (Amber Caution) (GV) YD 1-2 Fail (Blue Advisory) (GV-SP/GIV-X) 50 HZ Power Fail, L-R (Blue Advisory) (GV-SP/GIV-X) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures B (O) Except for ER operations, aeroplane may be dispatched with one (1) channel inoperative provided aeroplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. B (O) Aeroplane may be dispatched with one inoperative yaw damper system provided the inoperative YAW DAMPER SERVO #1: POP, D-6 or YAW DAMPER SERVO #2: CPOP, D-6 circuit breaker is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized. C (O) Aeroplane may be dispatched provided: a) L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Flight crew brief passengers on items that are inoperative with the failure of the power source for cabin entertainment, and c) Backup battery is available if EFB is used. PAGE NO: Operational Procedures Flight crew will ensure airplane is operated in accordance with AFM Limitations in the event the operative Yaw Damper fails. Flight crew will ensure inoperative servo YAW DAMPER SERVO #1: POP, D-6 or YAW DAMPER SERVO #2: CPOP, D-6 circuit breaker is pulled and collared. Flight crew will pull and collar affected L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker. Flight crew will brief the passengers on the items that are inoperative with the failure of the power source for cabin entertainment.

349 EUROPEAN AVIATION SAFETY AGENCY MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES / MANUAL AIRCRAFT: GULFSTREAM G-V, GV-SP, GV-SP (G550), GV-SP (G500), GIV-X, GIV-X (G450), GIV-X (G350) CAS Message 60 HZ Power Fail, L-R (Blue Advisory) (GV-SP/GIV-X) 60HZ PWR FAIL, L-R (Blue Advisory) (GV) MMEL REV. NO: 1 MMEL DATE: MOP REV. NO: 1 MOP DATE: Limitations and/or Procedures C (O) Aeroplane may be dispatched provided: a) Affected L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Flight crew brief passengers on items that are inoperative with the failure of the power source for cabin entertainment, and c) Backup battery is available if EFB is used. C (O) Aeroplane may be dispatched provided: a) Affected L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, b) Flight crew brief passengers on items that are inoperative with the failure of the power source for cabin entertainment, and c) Backup battery is available if EFB is used. PAGE NO: Operational Procedures Flight crew will pull and collar affected L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker. Flight crew will brief the passengers on the items that are inoperative with the failure of the power source for cabin entertainment. Flight crew will pull and collar affected L FREQ CONV: Left PDB or R FREQ CONV: Right PDB circuit breaker. Flight crew will brief the passengers on the items that are inoperative with the failure of the power source for cabin entertainment.

350 EUROPEAN AVIATION SAFETY AGENCY Gulfstream Aerospace P.O. Box 2206, M/S SW7 Savannah, GA Attention: Flight Crew Technical Information