AIRCRAFT SPECIFICATION SUMMARY. Airbus A

Transcription

1 AIRCRAFT SPECIFICATION SUMMARY Airbus A GENERAL AIRCRAFT INFORMATION AND OPERATIONAL DATA Aircraft: Manufacturer: Engines: APU: Build Year: MSN: Max Thrust (each): Airbus A Airbus Industries CFM 56-5C4 Honeywell GTCP C February lbs AIRFRAME DATA Airframe Cycles: Airframe Hours: 9,591 50,173 Canoga Capital Corp: Suite 15, 1st Floor, Oliaji Trade Centre, Francis Rachel Street, PO Box 1004,

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3 PERFORMANCE Maximum Cruise Altitude: Maximum Speed: Mach.86 Range with maximum pax: km DIMENSIONS Length: m Height: m Fuselage Diameter: 5.64 m Cabin Length: m Wingspam: m WEIGHTS Max Take-Off Weight: 275,581 Kgs / 606,280 Lb Max Taxi Weight: 276,483 Kgs / 608,264 Lbs Max Landing Weight: 192,406 Kgs / 423,294 Lb Max Zero Fuel Weight: 181,383 Kgs / 399,043 Lb Operating Empty Weight: 126,888 Kgs / 279,153 Lb Fuel Capacity: US Gallons

4 CABIN CONFIGURATION Seating Configuration Current Seating: 15 VIP First Class Seats Full 180 degree lying bed 70 Business Class Seats 127 Economy Class Seats Satellite Phone / WIFI / VISIO SYSTEM / FLAT SCREENS The Interior design has been customized by Envergure Design France It has reached the highest standards of design, engineering and workmanship with the production of this interior of best quality. Great care has been taken in selecting and matching finishes and colours. A rounded look has been applied to increase the feeling of comfort and softness, which is produced by the mix of beige colored seats and cushions. INSPECTION DATA Check Type Last Accomplished Interval Next Due 4C Check In Progress 730 Days / 10,000 Hrs 60,173 FH Sabena Technics - France June Years Check In Progress 2,190 Days June 2021 Sabena Technics - France 12 Years Check 37,894 FH / 6,378 FC 4,380 Days 29 March April 2009

5 POWERPLANT INFORMATION Type CFM56-5C4 Engine Thrust: 34,000 Lbs No.1 Position No.2 Position Serial No: Serial No: Total Hours: 42,996 FH Total Hours: 38,353 FH Total Cycles: 7,533 FC Total Cycles: 6,671 FC Date of LSV: 01 Dec 2011 Date of LSV: 20 Mar 2012 Hours Since LSV: 1,571 FH Hours Since LSV: 2,134 FH Cycles Since LSV: 376 FC Cycles Since LSV: 491 FC Cycles remaining: 4,570 FC Cycles remaining: 2,294 FC First Limiter: HPT Rotor Disk First Limiter: HPC Stage 3 Disk No.3 Position No.4 Position Serial No: Serial No: Total Hours: 48,507 FH Total Hours: 51,731 FH Total Cycles: 7,839 FC Total Cycles: 9,296 FC Date of LSV: 26 June 2009 Date of LSV: 16 Dec 2011 Hours Since LSV: 12,649 FH Hours Since LSV: 3,198 FH Cycles Since LSV: 1,942 FC Cycles Since LSV: 657 FC Cycles remaining: 4,161 FC Cycles remaining: 3,903 FC First Limiter: HPT Rotor Disk First Limiter: HPT Rear Shaft APU Manufacturer Honeywell Hours Since New 18,388 AH Serial Number R-370C Cycles Since New 15,842 AC Model GTCP C Hours Since LSV 6,354 AH LSV Date 31 May 2007 Cycles Since LSV 9,356 AC LANDING GEAR INFORMATION LH Main Nose Gear RH Main Centre Manufacturer: Messier Dowty Messier Bugatti Messier Dowty Messier Dowty Part No: D Serial No: MDL-252 B257 MDL-252 DCL251/02 Hours Since New: 50,172 TTH 50,172 TTH 50,172 TTH 41,854 TTH Cycles Since New: 9,591 TTC 9,591 TTC 9,591 TTC 7,032 TTC Last Done: 03 April March April July 2010 Next Due: 03 April March April July 2020 TBO 3,650 Days 3,650 Days 3,650 Days 3,650 Days 17,000 FC 17,000 FC 17,000 FC 17,000 FC

6 CABIN Galleys: 9 Lavatory: 9 Seats 15 VIP First Class Seats Full 180 degree lying bed 70 Business Class Seats 127 Economy Class Seats Total Seats 212 AVIONICS SUMMARY 22 Auto Flight Manufacturer Qty P/N FMGEC - Flight Management, Guidance and Envelope Computer Thales 2 C13039AA01 FCU Flight Control Unit Thales 1 C19266BA01 MCDU Multipurpose Control Display Unit Thales 3 C12849AA01 23 Communications HF Transceiver Collins VHF Transceiver Collins SDU SATCOM Data Unit Honeywell CVR Cockpit Voice Recorder TEAM 1 AP Audio Management Unit / Selcal Decoder TEAM 1 AMU3514CS01 Automatic ELT with External Antenna installed YES Flight Deck Door Camera System installed YES 31 Indicating and Recording FDR Flight Data Recorder Sagem 1 AP FDIU Flight Data Interface Unit SFIM 1 ED43B1D7 DMU Data Management Unit Honeywell Navigation ADIRU Air Data/Intertial Reference Unit Litton Ground Porximity Warning System Honeywell Weather Radar Transceiver Collins Windshear Installed? Reactive / Predictive YES TCAS Computer Collins ATC Mode S Transponder Collins DME Distance Measuring Equipment Interrogators Collins

7 Marker Beacon Transceiver Collins MMR Multi-Mode Receiver Collins GPS Navigation Installed YES Radio Altimeter Transceiver Collins ADF Receiver Collins Central Maintenance System (CMS) Multifunction Printer Thales 1 K282AAM Information Systems ATSU Air Traffic Services Unit Airbus 1 LA2T0G20503B040