BOMBARDIER GLOBAL EXPRESS XRS #9332 2010 Bombardier Global XRS Entered into Service: May 2010 Serial Number: 9332 Total Time Since New: 886 Hours Cycles: 365
GENERAL INFORMATION Beautiful 13 passenger interior Delivery Date: 14 th May 2010 Aircraft enrolled in CAMP system ENGINES Rolls-Royce BR700-710A2-20 Honeywell RE220 (APU) APU: 859 TSN & 678 CSN Engines enrolled in Rolls-Royce Corporate Care ADDITIONAL HIGHLIGHTS/OPTIONS Compliance with EU OPS 1 requirements Flight observer seat Securaplane Security System Electronic Flight Bag Installation Quick Access Recorder Additional Refuel/Defuel Control Panel Addition of Logo Light Provision for complete towbar assembly in AFT equipment bay Spare Nose wheel mounting provision in AFT equipment bay Combined Jacking Equipment Provisions in AFT equipment bay APU hour meter option Additional heater outlets for ground use EXTERIOR White with four design stripes using PRC Desoto & Sherwin Williams paints. AVIONICS Rockwell Collins SAT-6100 with two HST-2100 High Speed Date channel with Wifi in cabin connectivity Iridium Telephone System EVS: Enhanced Vision System Honeywell Primus 2000 XP Integrated Avionics System Honeywell 6-Tube Electronic Flight Instrument System (EFIS)/Engine Instrument and Crew Advisory System (EICAS) using DU-870 by 7-inch colour displays Honeywell Triple integrated Flight Management Systems Honeywell Navigation Data Base Data Loader (USB) Honeywell Dual Global Positioning System (GPS) Honeywell Triple IC-800 Integrated Avionics Computers (IAC); built in EFIS reversionary capability and fault warning redundancy - combines the functions of five major subsystems Triple Micro Air Data Computers (MADC) Triple Inertial Reference Systems (IRS) Quad DA-810 Data Acquisition Units (DAU) Honeywell Weather Radar - Dual control heads Honeywell LSZ-860 Lightning Sensor System (LSS) Honeywell Dual Integrated Nav./Com/Ident. Radios - VOR/ILS/MKR, ADF, DME, VHF Comm, Mode 'S' Diversity Transponder. Compliance with European 8.33 khz channel spacing requirements Honeywell RCZ-833 3rd VHF Transceiver Central Aircraft Information Maintenance System (CAIMS) Miltope Printer TP-4840 TCAS RT-950 Traffic Alert and Collision Avoidance System Dual HF Comm Selective Calling (SELCAL) System Dual Radar Altimeter Cockpit Voice Recorder (CVR) Digital Flight Data Recorder (DFDR) Enhanced Ground Proximity Warning System (EGPWS) Artex 406MHz Emergency Locator Transmitter (ELT) Thales Head-up Display Airborne Data Link System Specifications are subject to verification upon inspection.
INTERIOR EQUIPMENT Global office with 3 handsets and Facsimile/Copier Unit. Wireless and LAN network for High speed data internet access. 230VAC, 3500VA inverter with international outlets located throughout the cabin. Rockwell Collins CES and Environmental Control System for each seat as appropriate. Speaker system with 10 speakers and 4 subwoofers in cabin Personal Entertainment Controls (13 each) 21,5 LCD Monitors (1 each) 24 LCD Monitors (1 each) 10,4 touch screen monitor in galley (1 each) Plug-In LCD Monitor Receptacle (9 each) Plug-In 10,4 LCD Monitor w/ side mount Arm (4 each) Dual CD/DVD Player (3 each) Between main cabin and cockpit features RH forward galley with a sink, hot/cold water faucet, split pop-out work surface, countertop with raised edge, illuminated glass storage racks, ice drawer, cold storage drawer and storage space. Appliances include a Nespresso Espresso/Cappuccino machine with hot water dispenser, a TIA high temperature oven and TIA microwave oven. On the opposite side of the Galley exists crew rest area which is equipped with 18,5 single seat. Crew rest is separated from galley and entrance area by curtain. FINISH The wide seats and divans are finished in Carlucci di Chivasso fabric and conference group double seats has fabric with Spinneybeck leather edge finishing. Cabin is complemented by Edelman Marble color leather headliner and Townsend Woven Leather Gnarled Pine color sidewalls. Wood paneling is of Pegasus Fig Walnut from Custom Plywood. All metal parts are Antique Nickel coated. Airshow 500 Cabin Display System CONFIGURATION The 13-passenger executive interior was designed for functionality and flexibility in mind with three seating areas. The forward area is separated from the galley area by a sliding door and contains 4ea 21 individual seats in double club arrangement with two pull out writing tables, 4ea receptacles for individual plug-in video monitors and a bulkhead-mounted 21,3 monitor. On the left side of the main cabin there is a 4-place conference group with 2ea 43,5 double seats and 2ea receptacles for plug-in video monitors, an adjustable-height dining table. The conference group can be configured as a double bed. AFT area of main cabin has been separated with sliding door from FWD cabin. On the right side of AFT section there is a 3 place 80 divan with berthing extension. On the left side of the AFT main cabin there is a 3 place 80 (only 2 places may be used during taxi, take-off and landing) divan with berthing extension and a bulkhead-mounted 24 monitor. Behind the seating area there is a large enclosed lavatory with vanity unit and storage space. The baggage compartment is accessible from the lavatory via a door. Inspection Status Inspection Frequency Last Done Due A 500 Hours 422 972 FH 2A 1000 Hours N/A FH 1000 FH 3A 1500Hours N/AFH 1500 FH C 15 Months 19-AUG-2011 12-NOV-2012 2C 30 Months N/A 12-NOV-2012 4C 60 Months N/A 12-MAY-2015 8C 120 Months N/A 12-MAY-2020 Warranty Coverage Green aircraft 5 Years Weights: Maximum Ramp: Maximum Takeoff: Maximum Zero Fuel: Fuel Capacity: 99,750 lbs 99,500 lbs 56,000 lbs 45,050 lbs Specifications are subject to verification upon inspection.
Entrance
Forward Galley
Forward Galley
Forward Cabin
Forward Cabin
Forward Cabin Details
Mid Cabin
Mid Cabin
Aft Cabin
Entertainment Facsimile machine Entertainment Controls & Phone Fwd Table Detail
Control Panel AFT Lavatory
Floorplan