OE-DLP CESSNA - FR 172 G ROCKET
|
|
|
- Beatrice Blake
- 7 years ago
- Views:
Transcription
1 C 172 ROCKET Operator: Fliegergruppe Wien im österreichischen AERO- Club A Bad Vöslau Flugplatz OE-DLP: SN: FR BJ Motornummer: R Continental D B 20 Prop Mc. Cauley D2A 34C 67 OE-DLP CESSNA - FR 172 G ROCKET Checkliste Bordexemplar Darf NICHT vom Flugzeug entfernt werden. PREFLIGHT INTERIOR+EXTERIOR Remove pitot cover Control lock removed and stowed Ignition OFF Electrical equipment OFF Master switch ON Check fuel gauges Pitot heat ON, check amp meter Check interior lights Exterior lights ON Check exterior lights Check Pitot heat temperature Exterior lights and pitot heat OFF Master switch OFF Fuel selector valve BOTH Fuel shutoff valve OPEN PREFLIGHT EXTERIOR Left main gear Wheel fairing Tire condition, pressure, position mark Brake, hydraulic line Left fuselage Antennas Baggage door Static port Tail Elevator & rudder (freedom of movement, hinges) Trim - tab Position light Right fuselage Static port Right main gear Wheel fairing Tire condition, pressure, position mark Brake, hydraulic line PREFLIGHT PROCEDURES Right wing Drain fuel sump Wing flap Aileron (freedom of movement, hinges, control linkage, security) Wing tip, position light Wing leading edge, top- and bottom surface Fuel filler cap Nose section Propeller surface Spinner Air inlets Nose gear Wheel fairing Tire condition, pressure, position mark Engine bay Engine oil level Drain fuel strainer Left wing Wing leading edge, top- and bottom surface Fuel filler cap Fuel vent line Pitot tube (cover removed) Stall warning Landing light Wing tip, position light Aileron (freedom of movement, hinges, control linkage, security) Wing flap Drain fuel sump ISSUE 11 Page 1 / ISSUE 11 Page 2 / 15
2 CHECK BEFORE ENGINE START 1 Preflight check... COMPLETED 1 2 Baggage and tow bar...secured 2 3 Doors... CLOSED + LOCKED 3 4 Seats and seatbelts... ADJUSTED 4 5 Parking brake... SET 5 6 Flight controls... CHECKED 6 7 Clock... SET 7 8 Altimeters... SET 8 9 All switches... OFF 9 10 Avionics (5)... OFF Circuit breakers... CHECKED Engine counter reading... NOTED Fuel selector valve... BOTH Fuel shutoff valve... OPEN Master switch...on Fuel quantity... CHECKED Rotating beacon...on Mixture...RICH Propeller...HIGH RPM Primer... AS REQUIRED Auxiliary fuel pump... LOW 21 ENGINE START PROCEDURE Throttle... OPEN 2,5 cm (FF 2 GAL) Propeller area...clear Starter... ENGAGE Oil pressure...rising Throttle RPM Auxiliary fuel pump... OFF CHECK AFTER ENGINE START 1 Oil pressure... CHECKED 2 Auxiliary fuel pump... CHECKED OFF 3 Engine instruments... CHECKED 4 Primer... LOCKED 5 Avionics (5)...ON 6 Nav aids and frequencies... SET 7 GPS... AS REQUIRED 8 Ampere meter...loading 9 Horizon and directional gyro... SET 10 Flaps... CHECKED FULL TRAVEL 11 Transponder... ALT (if required) DURING TAXI Check brakes Check flight instruments BEFORE TAKE OFF CHECK 1 Parking brake... SET 2 Cabin doors + windows... CLOSED and LOCKED 3 Fuel selector valve... BOTH 4 Flight controls... CHECKED 5 Elevator trim... SET 6 Horizon, directional gyro, altimeters...rechecked 7 Flight instruments... CHECKED RUN UP PROCEDURE Throttle RPM Magnetos... checked max 50 RPM difference Propeller... cycle once, then HIGH 8 Engine Instruments... CHECKED 9 Ampere meter Generator Switch OFF - ON... CHECKED 10 Suction gauge... 4,6 5,4 in. Hg 11 Flaps... SET for TKOF 12 Pitot Heater... AS REQUIRED 13 Transponder...ALT 14 Parking brake... RELEASED ISSUE 11 Page 4 / ISSUE 11 Page 5 / 15
3 LINE UP PROCEDURE Landing light... on Approach sector... clear Runway... identified Gyro... check runway heading AFTER TAKE-OFF PROCEDURE After passing safe altitude: Flaps... up Throttle...25 inch RPM RPM Mixture...13 Gal Landing light... off DESCENT / APPROACH CHECK 1 Landing data...received 2 Altimeter... SET 3 COM / NAV... SET 4 Gyro... SET 5 Fuel selector valve... BOTH BEFORE LANDING PROCEDURE Throttle...15 inch Propeller RPM Mixture...rich Downwind, latest base leg: Flaps...10 Landing light...on On final: Flaps... as required Propeller... high RPM GO AROUND PROCEDURE Propeller and throttle... FULL Flaps...20 Then: Flaps... slowly up Continue with take-off profile CLIMB TO CRUISE CHECK 1 Landing light... CHECKED OFF 2 Flaps...CHECKED UP Flaps 10 Landing light on PERIODICALLY DURING CRUISE Fuel Radio Engine Direction Altitude ISSUE 11 Page 6 / ISSUE 11 Page 7 / 15
4 AFTER LANDING CHECK (when reaching taxi speed) 1 Flaps... UP 2 Transponder... SBY 3 Pitot heat... OFF 4 Landing / Taxi light... AS REQUIRED PARKING CHECK 1 Parking brake... AS REQIRED 2 ELT ,5 CHECKED 3 GPS... CHECK TRIP TIME 4 Avionics (5)... OFF 5 Landing / Taxi light... OFF 6 Ignition grounding (momentarily OFF)... CHECKED 7 Mixture... IDLE CUT OFF 8 Ignition... OFF 9 Rotating beacon... OFF 10 Master switch... OFF 11 Fuel shutoff valve... CLOSED 12 Engine counter reading... NOTED 13 Control wheel lock... INSTALLED 14 Pitot cover... INSTALLED Emergency Landing... page 8 Engine Fail... page 8 Engine Roughness... page 9 Low Oil Pressure... page 9 Engine Fire in Flight... page 9 Engine Fire on Ground...page 10 Electrical Fire in Flight...page 10 Excessive Electrical Charge...page 11 Insufficient Electrical Charge...page 11 EMERGENCY LANDING 1 Flaps... UP 2 Airspeed mph 3 Mixture... IDLE CUT OFF 4 Fuel shutoff valve... CLOSED 5 All switches except Master... OFF 6 Ignition... OFF 7 ATC... MAYDAY CALL 8 Flaps... AS REQUIRED 9 Master switch... OFF Before Touchdown: 10 Cabin Doors...UNLATCHED ENGINE FAIL 11 Airspeed mph 12 Fuel quantity... CHECKED 13 Fuel selector valve... FULLER TANK 14 Mixture... CHECKED 15 Fuel flow... CHECKED 16 Auxiliary fuel pump... ON if necessary 17 Primer... FULL IN + LOCKED 18 Ignition... PROPER POSITION or START If no success: continue with EMERGENCY LANDING Checklist ISSUE 11 Page 8 / ISSUE 11 Page 9 / 15
5 ENGINE ROUGHNESS 1 Magnetos...CHECK LEFT and RIGHT 2 Better magneto... SELECT 3 Mixture... LEAN AS REQUIRED If engine still rough: 4 Magnetos... BOTH 5 Mixture...RICH LOW OIL PRESSURE 1 Oil temperature... CHECK If oil temperature normal: If total loss of pressure and/or oil temperature high: 2 Power... REDUCE Forced landing ENGINE FIRE IN FLIGHT 1 Mixture... IDLE CUT OFF 2 Fuel shutoff valve... CLOSED 3 ATC... MAYDAY CALL 4 Airspeed MPH 5 Cabin heater and defroster... OFF Forced emergency landing: 6 Airspeed mph 7 Ignition... OFF 8 Flaps... AS REQUIRED 9 Master switch... OFF Before Touchdown: 10 Cabin Doors...UNLATCHED ENGINE FIRE ON GROUND Crank engine If engine starts: 1 Throttle RPM for several minutes 2 Engine... SHUT DOWN Discontinue operation If engine does not start: Continue cranking 3 Throttle...FULL OPEN Call for fire assistance 4 Auxiliary fuel pump... OFF 5 Fuel shutoff valve... CLOSED 6 Mixture... IDLE CUT OFF 7 Ignition... OFF 8 Master switch... OFF 9 Parking brake... RELEASED Evacuate - Extinguish ELECTRICAL FIRE IN FLIGHT 1 Master switch... OFF 2 Cabin heat and ventilation... CLOSED If electrical power required execute isolation procedure : 3 All switches (except ignition)... OFF 4 Circuit breakers... CHECKED Leave a faulty circuit deactivated 5 Master Switch...ON 6 Select switches ON successively to isolate faulty circuit... Leave faulty circuit deactivated When fire definitely extinguished: 7 Cabin heat and ventilation... AS REQUIRED ISSUE 11 Page 10 / ISSUE 11 Page 11 / 15
6 IMPORTANT DATA AND LIMITATIONS EXCESSIVE ELECTRICAL CHARGE (more than 2 needle widths after 30 min. flight time) 1 Generator switch (right half of master)... OFF 2 Electrical load...reduce NONESSENTIAL If necessary: 3 Generator...ON for limited periods During night before flaps and landing light required: 4 Generator...ON INSUFFICIENT ELECTRICAL CHARGE 1 Generator switch (right half of master)... OFF 2 Electrical load...reduce NONESSENTIAL OPERATING SPEEDS Mph Kt Best gliding angle (Flaps 0 ) Best angle of climb (V X ) 70/85 61/74 Best rate of climb (V Y ) Cruising climb speed Rotating speed Max. flap speed (V FE ) Landing speed Flaps Landing speed Flaps Stalling speed (V S0 ) Stalling speed (V S1 ) Max. cruising speed (V NO ) Never exceed speed (V NE ) Manoeuvring speed (V A ) Max. turbulence speed POWERSETTING and CRUISING SPEEED Press Alt Cruise TAS (mph/kt) 65% 55% 65% 75% RPM MP USG/hr / / / , / / / ,5 10, / / , / / ,5 10,0 Cons. 8,6 G/hr 10 G/hr 11,4 G/hr Endurance 05:20 hrs 04:35 hrs 04:01 hrs LIMITATIONS Max. TKOF RPM Max. cruise RPM Max. fuel on board Max. usable fuel 2800 RPM 2600 RPM 52 USG 46 USG 125 kp Max. TKOF weight Empty weight Max. load incl. fuel Max. load with full tank Max. baggage weight 1157 kp 731 kp 426 kp 301 kp 91 kp ISSUE 11 Page 12 / ISSUE 11 Page 13 / 15
7 GNS 430 TAKE OFF BRIEFING TAKE OFF BRIEFING GPS ANNUNCIATOR INTG TERM APP MSG NORMALSTART OF RUNWAY. CROSSWINDCOMPONENT...KT FROM... VLOC GPS CDI WPT OBS AUTO OBS LAMP TEST ROTATE BY...KT BEFOR / AFTER MID FIELD INDICATOR INITIAL CLIMB..KT UNTIL... FEET THEREAFTER...KT LANDINGAREA.... OBSTACLES ARE.. EMERGENCYLANDING MAX ANGLE 45 LEFT / RIGHT IN CASE OF EMERGENCY OR FIRE BEFOR TAKE OFF 1. POWER IDLE 2. BREAKS FULL APPLY 3. INFORM ATC IN CASE OF EMERGENCY AFTER TAKE OFF 1. SPEED 70 KNOTS OR.. 2. MIXTURE; FUELSELECTOR; IGNITION OFF 3. FLAPS FULL 4. MASTERSWITCH OFF 5. DOORS UNLOCK ISSUE 11 Page 15 / ISSUE 11 Page 14 / 15
FLYBLOCKTIME PA-28-140/160 Aircraft Type Checkout and Currency Quiz. NOTE: There may be one or more correct answers to each question.
FLYBLOCKTIME PA-28-140/160 Aircraft Type Checkout and Currency Quiz Pilot s Name Date NOTE: There may be one or more correct answers to each question. 1 ) The engine in a PA-28-140/160 is a A. Continental
CESSNA 172 CHECKLIST TAXI PRE-EXTERNAL CHECKS. 1. Lights - As required 2. Brakes - CHECK 3. Rolling Instruments Check - L/R
CESSNA 172 CHECKLIST PRE-EXTERNAL CHECKS TAXI 1. Wing & Engine covers - REMOVED 2. Control lock - REMOVED 3. Trim Check - Full Movement 4. Master - BATTERY ONLY - On 5. Flaps - Down to 20 Degrees 6. Lights
King Air C90A. Speeds (KIAS)
King Air C90A Speeds (KIAS) V MCA 90 V SSE 97 V X 101 V Y 111 V XSE 100 V YSE 107 V A 169 V REF 100 V MO 208 V FE 178 35% 137 100% V LE 156 129 Retraction only Other 95 Balked landing climb 125 Glide 161
BOMBARDIER CRJ700. Bombardier CRJ700 Aircraft Reference
Bombardier CRJ700 Aircraft Reference V 1 Takeoff Decision Speed, dry runway 50,000 lbs, (flaps 8) 144 KIAS 50,000 lbs, (flaps 20) 134 KIAS V R Rotation Speed, dry runway 50,000 lbs, (flaps 8) 144 KIAS
Super King Air 200. Speeds (KIAS)
Super King Air 200 Speeds (KIAS) V MCA 86 V SSE 104 V X 100 V Y 125 V XSE 115 V YSE 121 V A 181 V REF 103 132 with no flap V MO 260 270 for old models M MO 0,52 0,48 for old models V FE 200 40% 146 100%
SINGLE ENGINE PISTON AEROPLANE ENDORSEMENT
SINGLE ENGINE PISTON AEROPLANE ENDORSEMENT ENGINEERING, DATA AND PERFORMANCE QUESTIONNAIRE FOR (Aeroplane make and model) Version 1 August 1996 Name: Endorsed by: (Signature/Name) ARN: ARN Satisfactorily
MULTI-ENGINE PISTON AEROPLANE ENDORSEMENT
MULTI-ENGINE PISTON AEROPLANE ENDORSEMENT ENGINEERING, DATA AND PERFORMANCE QUESTIONNAIRE FOR---------------------------------------------------------------------------------------------------------- (Aeroplane
MULTI-ENGINE TURBO-PROP AEROPLANE ENDORSEMENT
MULTI-ENGINE TURBO-PROP AEROPLANE ENDORSEMENT ENGINEERING, DATA AND PERFORMANCE QUESTIONNAIRE FOR (Aeroplane make & model) Version 1 -August 1996 Name: ARN. Endorser: ARN: (Signature/Name) 1 The endorsement
Multi Engine Oral Exam Questions
Multi Engine Oral Exam Questions 1. What are the requirements for a multi-engine rating? 2. What is the max rated horse power at sea level? At 12,000 msl? 3. What is the rated engine speed? 4. What is
Lancair Legacy Annual Condition Inspection Checklist
Lancair Legacy Annual Condition Inspection Checklist Performed by: Completion Date: Complete Maintenance/Inspection Item Comments Pre-Inspection Research AD and Service bulletins Inspect entire airframe
File Number MDRA C20 MANUAL of PROCEDURES for INSPECTION of COMPOSITE AMATEUR-BUILT AIRCRAFT, INSPECTION AND TECHNICAL INFORMATION RECORD
File Number MDRA C20 MANUAL of PROCEDURES for INSPECTION of COMPOSITE AMATEUR-BUILT AIRCRAFT, INSPECTION AND TECHNICAL INFORMATION RECORD GENERAL Section 1.4 FINAL INSPECTION 1. Have all re-inspection
SINGLE ENGINE TURBO-PROP AEROPLANE ENDORSEMENT
SINGLE ENGINE TURBO-PROP AEROPLANE ENDORSEMENT ENGINEERING, DATA AND PERFORMANCE QUESTIONNAIRE FOR (Aeroplane make & model) Version 1-31 August 1996 Name: Endorser: (Signature/Name) Satisfactorily Completed
MULTI-ENGINE PISTON AEROPLANE ENDORSEMENT ENGINEERING, DATA AND PERFORMANCE QUESTIONNAIRE
CAAP 5.23-1(1): Multi-engine Aeroplane Operations and Training 117 APPENDIX D TO CAAP 5.23-1(1) MULTI-ENGINE PISTON AEROPLANE ENDORSEMENT ENGINEERING, DATA AND PERFORMANCE QUESTIONNAIRE FOR (Aeroplane
MULTI-ENGINE TURBO-PROP AEROLANE ENDORSEMENT
CAAP 5.23-1(1): Multi-engine Aeroplane Operations and Training 133 Appendix E to CAAP 5.23-1(1) MULTI-ENGINE TURBO-PROP AEROLANE ENDORSEMENT ENGINEERING, DATA AND PERFORMANCE QUESTIONNAIRE FOR (Aeroplane
General Characteristics
This is the third of a series of Atlantic Sun Airways CAT C pilot procedures and checklists for our fleet. Use them with good judgment. Note, the start procedures may vary from FS9 Panel to Panel. However
This is the fourth of a series of Atlantic Sun Airways CAT B pilot procedures and checklists for our fleet. Use them with good judgment.
This is the fourth of a series of Atlantic Sun Airways CAT B pilot procedures and checklists for our fleet. Use them with good judgment. Dimensions: Wing Span: 112 ft 7 in Length: 129 ft 6 in Height: 41
2013 Airborne Aviation Pty Ltd www.airborne-aviation.com.au
Aircraft Information Booklet Cessna 182T VH-SDN Last revised: 11 November 2013 2013 Airborne Aviation Pty Ltd www.airborne-aviation.com.au THIS PAGE INTENTIONALLY LEFT BLANK Contents Aircraft Overview
This is the third of a series of Atlantic Sun Airways CAT B pilot procedures and checklists for our fleet. Use them with good judgment.
This is the third of a series of Atlantic Sun Airways CAT B pilot procedures and checklists for our fleet. Use them with good judgment. Dimensions: Span 107 ft 10 in Length 147 ft 10 in Height 29ft 7 in
Cherokee Archer II Pilot s Operating Handbook
Cherokee Archer II Pilot s Operating Handbook Cherokee Archer II PA-28-181 Handbook Part No. 761 624 New Piper Aircraft And The Notre Dame Pilot Initiative Partners in Aviation Education Not to be used
FLIGHT TRAINING (AEROPLANE) BASED ON JAR FCL - PPL(A) FLIGHT INSTRUCTION Syllabus
FLIGHT TRAINING (AEROPLANE) BASED ON JAR FCL - PPL(A) FLIGHT INSTRUCTION Syllabus for MARSPOLAR, DUBAI UAE Exercise 1 Familiarisation with the aeroplane characteristics of the aeroplane cockpit layout
PILOT OPERATING HANDBOOK FOR ROCKWELL TURBO COMMANDER 690B
PILOT OPERATING HANDBOOK FOR ROCKWELL TURBO COMMANDER This manual was compiled for unique and exclusive use with Rockwell Turbo Commander from ENEAIONES SIMULATIONS GROUP. The information herein contained
VFR Day Emergencies - C172R
Pilot Level: References: Note: VFR Day Emergencies - C172R Student Pilot. FAA-H-8083-3A, Chapter 16, Federal Aviation Regulations, Cessna 172R PIM, Aeronautical Information Manual, King Schools (DVDs):
Light Sport West Standard Flight Training Procedures for N110GX (Remos GX, 100 H.P.)
Light Sport West Standard Flight Training Procedures for N110GX (Remos GX, 100 H.P.) Welcome to Light Sport West! Thank you for giving us the opportunity to provide all of your flight training needs. Our
CUB CRAFTERS, INC. CC11-160 PILOT S OPERATING HANDBOOK AND FLIGHT TRAINING SUPPLEMENT
CUB CRAFTERS CUB CRAFTERS, INC. PILOT S OPERATING HANDBOOK AND FLIGHT TRAINING SUPPLEMENT Airplane Serial Number: Airplane Registration Number: This airplane is approved as a special light-sport category
Cessna Grand Caravan Pilot s Technical Examination
Cessna Grand Caravan Pilot s Technical Examination Version 1.0 2003-05-13 Candidate Name Licence class Private/Commercial/ATP Examiner Licence number Name Licence number Capacity Centre Date 200 -- --
The SeaRey - An Introduction
The SeaRey - An Introduction Welcome to the beautiful Progressive Aerodyne SeaRey. The SeaRey is a very special aircraft. Created by a small team of engineers the SeaRey is perhaps the ultimate kit built
FLIGHT REFERENCE CARDS
Card 1 (AL 18) Issue 1 October, 1973 (AL 18, March 1992) AP 101B-3801-14 FLIGHT REFERENCE CARDS BULLDOG SERIES 120 NORMAL DRILLS Prepared by Royal Air Force Handling Squadron Amended by FlyLogical for
FLIGHT CONTROLS 1. GENERAL 2. MAIN COMPONENTS AND SUBSYSTEMS ROLL CONTROL. Smartcockpit.com BOEING 737 SYSTEMS REVIEW Page 1
Smartcockpit.com BOEING 737 SYSTEMS REVIEW Page 1 FLIGHT CONTROLS 1. GENERAL The primary flight controls, ailerons, elevators and rudders, are hydraulically powered. Hydraulic power is provided from hydraulic
TYPE CERTIFICATE DATA SHEET Nº EA-2011T03 Type Certificate Holder: COSTRUZIONI AERONAUTICHE TECNAM S.r.l. Via Tasso, 478 80127 - Napoli Italy
TYPE CERTIFICATE DATA SHEET Nº EA-2011T03 Type Certificate Holder: COSTRUZIONI AERONAUTICHE TECNAM S.r.l. Via Tasso, 478 80127 - Napoli Italy EA-2011T03-02 Sheet 01 TECNAM P2006T 04 May 2012 This data
Cessna 172SP & NAV III Maneuvers Checklist
Cessna 172SP & NAV III Maneuvers Checklist Introduction Power Settings This document is intended to introduce to you the standard method of performing maneuvers in Sunair Aviation s Cessna 172SP and NAV
AIRCRAFT GENERAL www.theaviatornetwork.com GTM 1.1 2005 1-30-05 CONTENTS
www.theaviatornetwork.com GTM 1.1 CONTENTS INTRODUCTION... 1.2 GENERAL AIRPLANE... 1.2 Fuselage... 1.2 Wing... 1.2 Tail... 1.2 PROPELLER TIP CLEARANCE... 1.2 LANDING GEAR STRUT EXTENSION (NORMAL)... 1.2
This section includes performance data on the King Air B200. Information consists of:
King Air B200 POH Pilot's Operating Handbook: This section includes performance data on the King Air B200. Information consists of: 1. Critical Airspeeds 2. Operating NOTAMS 3. Fuel Loading Formula Checklists:
S-Tec System Thirty Autopilot
Cirrus Design Section 9 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for S-Tec System Thirty Autopilot When the S-Tec System Thirty Autopilot is installed in the Cirrus
ECO1. Efficient flight dynamics
ECO1 Efficient flight dynamics Experience ECO1. Large cumulus clouds lie next to you, like a string of pearls. You lower the nose and feel the immediate acceleration. When the speed is 300 km/h, you pull
DA20-100 Katana 4X Manual. This Chapter provides description and operation of the airplane and its systems.
7.0 OF THE AIRPLANE AND ITS SYSTEMS 7.1. INTRODUCTION This Chapter provides description and operation of the airplane and its systems. 07
MCR-01 Ultralight. AFS-design. Andreas Meyer
MCR-01 Ultralight AFS-design Andreas Meyer Summary AFS-design brings a excellent rendition of Dyn'Aero MCR-01 Ultralight. The MCR 01 Sportster ULC(LSA) Ultralight is a side by side two-seater airplane
Municipal Airport 1410 Arizona Place S.W. Orange City, IA 51041-7453. www.angelaircraft.com aac@angelaircraft.com 712.737.3344
Municipal Airport 1410 Arizona Place S.W. Orange City, IA 51041-7453 www.angelaircraft.com aac@angelaircraft.com 712.737.3344 PERFORMANCE SPECIFICATIONS POWERPLANT PROPELLER Lycoming IO-540 300 HP @2700
NOTICE. Dec 2/96 CESSNA AIRCRAFT COMPANY ORIGINAL ISSUE - 2 DECEMBER 1996
NOTICE AT THE TIME OF ISSUANCE, THIS INFORMATION MANUAL WAS AN EXACT DUPLICATE OF THE OFFICIAL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL AND IS TO BE USED FOR GENERAL PURPOSES
ELECTRICAL. Primary electrical power is provided by two engine driven generators which supply three-phase, 115 volt 400 cycle alternating current.
Smartcockpit.com BOEING 737 SYSTEMS REVIEW Page 1 ELECTRICAL 1. GENERAL Primary electrical power is provided by two engine driven generators which supply three-phase, 115 volt 400 cycle alternating current.
CHAPTER 11 MARKING AND PLACARDS
CHAPTER 11 MARKING AND PLACARDS P/N 135A-970-100 Chapter 11 REVISION E Page 1 of 38 Copyright 2010 All rights reserved. The information contained herein is proprietary to Liberty Aerospace, Incorporated.
SD3-60 AIRCRAFT MAINTENANCE MANUAL AND MOORING - GENERAL
AMM 10-00-00 1.0.0.0PARKING AND MOORING - GENERAL 1. General Information on parking and mooring the aircraft in normal conditions is given in the following sections: - Parking (Refer to 10-11-00, pb201.)
B777. Landing Gear DO NOT USE FOR FLIGHT
B777 Landing Gear DO NOT USE FOR FLIGHT Introduction The airplane has two main landing gear and a single nose gear. The nose gear is a conventional steerable two wheel unit. Each main gear has six wheels
CIRRUS AIRPLANE MAINTENANCE MANUAL
UNSCHEDULED MAINTENANCE CHECKS 1. DESCRIPTION The following describes those maintenance checks and inspections on the aircraft which are dictated by special or unusual conditions which are not related
Pilot operating handbook. And. Flight operating supplement. AEROPRO + EuroFOX Aviation. EuroFOX
` AEROPRO, Production of UL Planes Dlha 126, 949 07 NITRA Slovakia www.aeropro.sk Pilot operating handbook And Flight operating supplement AEROPRO + EuroFOX Aviation EuroFOX The aircraft design has been
CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC
CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC 62 001 - L 200 D Revision 3 Aircraft Industries, a.s. L 200 D 05.09.2005 TYPE CERTIFICATE DATA SHEET No. 62 001 - L 200 D This data sheet which is a part
AIRCRAFT PERFORMANCE Pressure Altitude And Density Altitude
Performance- Page 67 AIRCRAFT PERFORMANCE Pressure Altitude And Density Altitude Pressure altitude is indicated altitude corrected for nonstandard pressure. It is determined by setting 29.92 in the altimeter
LANDING GEAR & BRAKES www.theaviatornetwork.com GTM 14.1 2005 1-30-05 CONTENTS INTRODUCTION... 14.2
www.theaviatornetwork.com GTM 14.1 CONTENTS INTRODUCTION... 14.2 GENERAL... 14.2 MAIN LANDING GEAR... 14.2 Landing Gear Latch Lever and Handle... 14.2 Landing Gear Pressure Gauge... 14.2 Landing Gear Warning
FLY SYNTHESIS STORCH HS-CL
STORCH HS-CL MAINTENANCE MANUAL (ALID FOR ROTAX 912 UL AND JABIRU 2200 ENGINES) 00 28/05/07 New manual issue Num. Date Description Issued erify Approvation REISION The FlySynthesis s.r.l. it reserves him
Multi-Engine Training And The PTS
Multi-Engine Training And The PTS GHAFI John Sollinger/Larry Hendrickson October 28, 2000 Overview FAR differences between original and add-on Multi-Engine PTS Training methods Common training scenarios
Compiled by Matt Zagoren
The information provided in this document is to be used during simulated flight only and is not intended to be used in real life. Attention VA's - you may post this file on your site for download. Please
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 3A12 Revision 77 CESSNA 172 172I 172A 172K 172B 172L 172C 172M 172D 172N 172E 172P 172F (USAF T-41A) 172Q 172G 172R 172H (USAF T-41A) 172S June
MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS Note: The scope of this Module should reflect the technology of aeroplanes pertinent to the A2 and B1.2 subcategory. 11.1 Theory of Flight
PILOT OPERATING HANDBOOK
ZODIAC 601XL / 601XLi / 650LS / 650LSi SLSA CONTINENTAL 0-200 100 H.P. PILOT OPERATING HANDBOOK REGISTRATION: SERIAL NUMBER: AMD Original date of issue: November 2009 Revision 2 March 2010 PILOT OPERATING
CENTRE EST AERONAUTIQUE
Identification : Aeroplane Type DR 1050M1 Sicile Record Serial No 579 Engine : Type Continental 0200A Serial No 20R-077 Propeller : Type Ratier FH 110-R Serial No 26 Registration : G-BAEE Flight Manual
SUPPLEMENTARY INFORMATION FOR FLIGHT STUDENTS
SUPPLEMENTARY INFORMATION FOR FLIGHT STUDENTS This pamphlet provides information to assist flight students in learning standardized procedures at the University of Oklahoma Aviation Department and guidance
TECNAM P2002JF. Specification & Description INTRODUCTION
SPECIFICATION & DESCRIPTION Pag. 1 TECNAM P2002JF Specification & Description INTRODUCTION INDROD UCTION This document is published for the purpose of providing general information for the evaluation of
Aviation Supplies & Academics, Inc. 7005 132nd Place SE Newcastle, Washington 98059-3153 www.asa2fly.com
The Pilot s Manual 1: Flight School Aviation Supplies & Academics, Inc. 7005 132nd Place SE Newcastle, Washington 98059-3153 www.asa2fly.com Originally published by Aviation Theory Centre 1990 1993. Fourth
TITLE 14 CIVIL AVIATION
CIVIL AIR REGULATIONS PART 4b-AIRPLANE AIRWORTHINESS TRANSPORT CATEGORIES CIVIL AERONAUTICS BOARD As amended to December 31, 1953 WASHINGTON, D.C. TITLE 14 CIVIL AVIATION Chapter 1 Civil Aeronautics Board
SERIOUS INCIDENT. Aircraft Type and Registration: No & Type of Engines: 2 SNECMA CFM 56-7B turbofan engines. Year of Manufacture: 1999
SERIOUS INCIDENT Aircraft Type and Registration: No & Type of Engines: Boeing 737-86N, SE-RHX 2 SNECMA CFM 56-7B turbofan engines Year of Manufacture: 1999 Date & Time (UTC): Location: Type of Flight:
2014 NIFA CRM Contestant Briefing Guide San Diego, California
2014 NIFA CRM Contestant Briefing Guide San Diego, California Region 2 SAFECON 2014 November 12 15 This document supports the 2014 NIFA Collegiate Cockpit Resource Management Simulation and is not for
ACCUMULATOR INSTALLATION
7001-7 ACCUMULATOR INSTALLATION BRAKE ACCUMULATORS I 308L93 Rae 7-59710 Issued 6-93 Printed in U.S.A 7001-8 Removal ACCUMULATOR VALVE 1. Park the machine on a level surface and lower the. loader bucket
ENGINE FIRE / SEVERE DAMAGE / SEPARATION ON TAKEOFF
ENGINE FIRE / SEVERE DAMAGE / SEPARATION ON TAKEOFF According to RYANAIR Procedures PF PM REMARKS Control the aircraft (FULL T/O thrust can be manually selected) Announce «ENGINE FAILURE» or «ENGINE FIRE»
Chapter 21 Air Conditioning
Chapter 21 Page Date: 8. December 1999 21 Page 1 Table of Contents 21-00-00 GENERAL...5 Description...5 Troubleshooting...6 Service and Maintenance...8 Removal / Installation...8 21-20-00 DISTRIBUTION...9
SECTION 23 05 93 TESTING, ADJUSTING, AND BALANCING FOR HVAC INTRODUCTORY INFORMATION
SECTION 23 05 93 TESTING, ADJUSTING, AND BALANCING FOR HVAC INTRODUCTORY INFORMATION The purpose of this guide specification is to assist the specifier in correctly specifying Mechanical System Testing
BE76 Beechcraft Duchess Maneuvers Checklist
BE76 Beechcraft Duchess Maneuvers Checklist Introduction Power Settings This document is intended to introduce to you the standard method of performing maneuvers in Sunair Aviation s Beechcraft Duchess
Cessna 172S. Flight Training Standardization Guide REVISION: ORIGINAL
Cessna 172S Flight Training Standardization Guide REVISION: ORIGINAL Contents Purpose... 4 Normal and Crosswind Takeoff and Climb... 5 Normal and Crosswind Landing... 6 Soft Field Takeoff and Climb...
LYCOMING OPERATOR S MANUAL SECTION 3 OPERATING INSTRUCTIONS
LYCOMING OPERATOR S MANUAL SECTION 3 Page General... 3-1 Prestarting Items of Maintenance... 3-1 Starting Procedures... 3-1 Cold Weather Starting... 3-3 Ground Running and Warm-Up... 3-3 Ground Check...
Basic Aviation Training Device
FLYIT SIMULATORS, Inc. Basic Aviation Training Device Model PHS - 1 FLYIT Simulators Inc. 5931Sea Lion Pl #110 Carlsbad, CA 92010 USA Revised on 10/30/2014 Page 1 of 53 Device Description and Overview
2009 Annual Inspection Airframe Logbook Entry
2009 Annual Inspection Airframe Logbook Entry N724MC Cessna 150L 150-72198 5,528.4 Engine Lycoming O-320-A2B RL-22173-27A 2,115.9 965.9 Propeller McCauley 1C172/TM-7456 E 8764 (Position) (Make and Model)
MEMO AIRBUS A319/A320/A321. SOP / Flow Pattern
MEMO AIRBUS A319/A320/A321 SOP / Flow Pattern F/O side only ( or ) A320 Flow Pattern SOP Visual Pattern Engine Out Memory Items Emergency procedures Laurent ALAPHILIPPE Page 1/18 Année 2011 Summary Memo
Cessna Citation 500/501 Pilot s Technical Examination
Cessna Citation 500/501 Pilot s Technical Examination Version 0.2 2003-09-28 Candidate Examiner Name Licence class Licence number Name Licence number Capacity Private/Commercial/ATP Centre Date 200 --
Microsoft Flight Simulator X Key Commands
Microsoft Flight Simulator X Key Commands SIMULATOR COMMANDS NOTE: Make sure Num Lock is OFF before using Num Pad combinations. Pause P or BREAK Full Screen Mode ALT + ENTER Menus (display/hide) ALT ATC
Cessna Skyhawk II / 100. Performance Assessment
Cessna Skyhawk II / 100 Performance Assessment Prepared by John McIver B.Eng.(Aero) Temporal Images 23rd January 2003 http://www.temporal.com.au Cessna Skyhawk II/100 (172) Performance Assessment 1. Introduction
TRAINING BULLETIN Fire Apparatus Pump Test
TOPIC: TRAINING BULLETIN Fire Apparatus Pump Test EFFECTIVE DATE: 05/06 DOC NO: TB081 CROSS REF: INTRODUCTION District Fire Apparatus Pump Testing is completed on an annual basis. Currently, pump testing
B 737 NG El ectrical
B737 NG Electrical Introduction Aircraft equipped with Single Battery Primary electrical power is provided by two engine integrated drive generators (IDGs) which supply three-phase, 115 volt, 400 cycle
Revision Number Revision Date Insertion Date/Initials 1 st Ed. Feb 01, 00 2 nd Ed. Jun 24, 02 3rd Ed. Feb 15, 07
List of Effective Pages * Asterisk indicates pages changed, added, or deleted by current revision. Retain this record in front of handbook. Upon receipt of a Record of Revisions revision, insert changes
OPERATING LIMITATIONS
OPERATING LIMITATIONS CERTIFICATION STATUS NOTICE CERTIFICATION AND OPERATIONAL LIMITATIONS ARE CONDITIONS OF THE TYPE AND AIRWORTHINESS CERTIFICATES AND MUST BE COMPLIED WITH AT ALL TIMES AS REQUIRED
The most exciting benefit of the GENESIS Conversion, by D Shannon is that it comes with a Maximum Gross Take-off Weight of 4000 lb.
Webster s Dictionary defines the word Genesis as forming, combining form meaning origination, creation, formation, evolution. In short, we have combined a number of our existing Bonanza modifications to
PRELIMINARY INVENTORY K0567 (KA1706, KA2285) DAN REX CORNWELL (1930- ) PAPERS [TWA]
![PRELIMINARY INVENTORY K0567 (KA1706, KA2285) DAN REX CORNWELL (1930- ) PAPERS [TWA]](/thumbs/33/15981195.jpg "PRELIMINARY INVENTORY K0567 (KA1706, KA2285) DAN REX CORNWELL (1930- ) PAPERS [TWA]")
PRELIMINARY INVENTORY K0567 (KA1706, KA2285) DAN REX CORNWELL (1930- ) PAPERS [TWA] This collection is available at The State Historical Society of Missouri Research Center- Kansas City. If you would like
Section 9. Pitot Static System. 1 of 6
1 of 6 ITOT STATIC SYSTEM General The pitot static systems operate the Air Speed Indicator, Vertical Speed Indicator and the Altitude Indicator for each pilot. In addition, fitted into the Co-pilot's system,
FLIGHT MANUAL. Bailey-Moyes DRAGONFLY
24.8.00 FLIGHT MANUAL Bailey-Moyes DRAGONFLY Manufactured by Moyes Microlites Pty Ltd. 173 Bronte Road Waverley 2024 NSW Australia Ph. +61 2 9387 5114 Fax + 61 2 9369 3342 Email moyes@zip.com.au Bailey-Moyes
Electro-Mechanical Landing Gear System. Landing Gear and Brakes
Electro-Mechanical Landing Gear System N O 2 D U A L F E D B U S LANDING RELAY 5A DOWN EMERGENCY EXTENSION DOWN LIMIT GROUND AIRBORNE DOWN LIMIT Landing Gear and Brakes DOWNLOCK HOOK ENGAGED GROUND AIRBORNE
AVIATION OCCURRENCE REPORT A98W0192 ENGINE FAILURE
Transportation Safety Board of Canada Bureau de la sécurité des transports du Canada AVIATION OCCURRENCE REPORT A98W0192 ENGINE FAILURE MARTINAIR HOLLAND N.V. BOEING 767-300 PH-MCI CALGARY INTERNATIONAL
Chapter 2. Basic Airplane Anatomy. 2008 Delmar, Cengage Learning
Chapter 2 Basic Airplane Anatomy Objectives Identify components of basic aircraft anatomy Understand aircraft size and weight categories List different types and examples of General aviation aircraft Military
The following information is an exert from THE CESSNA 182 TRAINING MANUAL, Oleg Roud and Danielle Bruckert
The following information is an exert from THE CESSNA 182 TRAINING MANUAL, Oleg Roud and Danielle Bruckert Model History We provide the following information to outline significant differences from an
Oral Preparation Questions
Oral Preparation Questions The oral section of the practical test is the time when you need to demonstrate your understanding of the various tasks listed in the practical test standards and the factors
Civil Aviation Authority Czech Republic
TCDS 27323-1958 L 60 Page 1 of 17 Civil Aviation Authority Czech Republic CAA CZ TYPE-CERTIFICATE DATA SHEET L 60 Type Certificate Holder: EVEKTOR, spol. s r.o. Letecká 1008 686 04 Kunovice Manufacturer:
Exam questions for obtaining aircraft licenses and ratings
Exam questions for obtaining aircraft licenses and ratings Subject: PPL (A) Flight performance and planning Revision 1 07.10.2009. Period of validity: 01 January 2010 th - 31 December 2010 th Belgrade
WATER AND WASTE SYSTEMS WATER AND WASTE SYSTEMS
WATER AND WASTE SYSTEMS Table of Contents Vol. 1 21--00--1 REV 56, Jan 31/03 CHAPTER 21 --- WATER AND WASTE SYSTEMS Page TABLE OF CONTENTS 21-00 Table of Contents 21--00--1 INTRODUCTION 21-10 Introduction
Maintenance manual DG-1000S. 0.1 Manual amendments No. Page Description Date 1 0.5, 0.6, 4.14-4.16 diagrams 7, 11, 12
Maintenance manual DG-1000S 0 General 0.1 Manual amendments No. Page Description Date 1 0.5, 0.6, 4.14-4.16 diagrams 7, 11, 12 Manual revision TN413/2 September 2003 2 0.6, diagrams 1 and 11 Manual revision
COSTRUZIONI AERONAUTICHE TECNAM S.R.L.
P2006 T COSTRUZIONI AERONAUTICHE TECNAM S.R.L. Costruzioni Aeronautiche Tecnam operates in two facilities. The Casoria facility is located adjacent to the Napoli Capodichino Airport and covers an area
Instruction Manual Specification:
Instruction Manual Specification: Wingspan: 1855mm (73 ) Length: 1970mm (77.5 ) Weight: 7.5-9Kg (Approx.) Radio: 6+ Channel (Required) Turbine: 50-100N (5-10Kg) (Recommended) Introduction Congratulations
Flight Manual. FM 250 Vampire. Flight Manual
Flight Manual FM 250 Vampire Flight Manual CONTENT SECTION PAGE 1. General 2. Limitations 3. Normal Procedures 4. Emergency Procedures 5. Performance 6. Airplane Handling, Service & Maintenance Information
Societe Aeronautique Normande. Saint-Martin Aerodrome. Bernay (Eure) JODEL DR1050 Ambassadeur INSTRUCTION MANUAL
Societe Aeronautique Normande Saint-Martin Aerodrome Bernay (Eure) JODEL DR1050 Ambassadeur INSTRUCTION MANUAL Re-created from a photocopy of the original Richard Hurst July 1999 CONTENTS Specification
Heating, Ventilation, Air Conditioning and Refrigeration (HVACR)
Heating, Ventilation, Air Conditioning and Refrigeration (HVACR) I. Demonstrate safety skills in typical HVACR work situations to NATE Core Installer Knowledge Areas for Technician Excellence for Safety
TAXI, TAKEOFF, CLIMB, CRUISE, DESCENT & LANDING
OPERATIONS MANUAL FLT CREW TRAINING COMMERCIAL LEVEL SIMULATIONS TAXI, TAKEOFF, CLIMB, CRUISE, DESCENT & LANDING Commercial Level Simulations www.commerciallevel.com 1 Disclaimer This manual is not provided
B777. Automatic Flight DO NOT USE FOR FLIGHT
B777 Automatic Flight DO NOT USE FOR FLIGHT 4.10 Automatic Flight-Controls and Indicators Mode Control Panel (MCP) A/T ARM L R IAS MACH HDG TRK V/S FPA ALTITUDE A/P F/D ON OFF CLB CON IAS LNAV VNAV AUTO
Flight Manual P92 ECHO & P92 ECHO/100 FLIGHT MANUAL. Warning. (ROTAX 912UL 81Hp or ROTAX 912ULS 100Hp engine ) MANUFACTURER : COSTRUZIONI AERONAUTICHE
/100 INTRODUCTION Flight Manual P92 ECHO & P92 ECHO/100 (ROTAX 912UL 81Hp or ROTAX 912ULS 100Hp engine ) MANUFACTURER : COSTRUZIONI AERONAUTICHE AIRCRAFT TYPE : P92 ECHO & P92 ECHO/100 SERIAL NUMBER :...
Over the Fire Line, All Over the Globe.
Over the Fire Line, All Over the Globe. 2 3 WHEN THE HEAT IS ON. AT-802F: The Most Efficient, Effective Air Tanker Flying. From the Americas, across Europe, through the Mediterranean, and around the world,
Flight Instruments. Chapter 7. Introduction. Pitot-Static Flight Instruments
Chapter 7 Flight Instruments Introduction In order to safely fly any aircraft, a pilot must understand how to interpret and operate the flight instruments. The pilot also needs to be able to recognize