GENERAL TECHNICAL SPECIFICAITON

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1 GENERAL TECHNICAL SPECIFICAITON AIRCRAFT TYPE Bombardier CL-600-2B19 RJ Series 200-LR SERIAL NUMBER 7457 COUNTRY OF REGISTRATION REGISTRATION NUMBER United States N655BR DATE OF MANUFACTURE December 9, 2000 ENGINE TYPE General Electric CF34-3B1 OPERATING WEIGHTS MAX TAXI (RAMP) WEIGHT MAX TAKE OFF WEIGHT MAX LANDING WEIGHT MAX ZERO FUEL WEIGHT FUEL CAPACITY MAX PAYLOAD 53,250 lb (24,154 kg) 53,000 lb (24,041 kg) 47,000 lb (21,319 kg) 44,000 lb (19,835 kg) 14,305 lb (6,489 kg) 13,100 lb (5,942 kg) INTERIOR CONFIGURATION SEATS 50 all economy GALLEYS One, located in forward cabin LAVATORIES One; located in aft cabin AIRCRAFT CURRENT STATUS Bombardier Aerospace, Tucson, Arizona following Mexicana Link Return From Lease : Adresse rcs.

2 AIRFRAME DATA IS EFFECTIVE AS OF: February 20, 2011 TOTAL HOURS 18,371 TOTAL CYCLES 20,782 CURRENT MAINTENANCE PROGRAM A- (A, 2A, 3A, 4A, 5A, 8A) EVERY 500 Flight Hours 5,000 HOUR (C-1) EVERY 5,000 Flight Hours 10,000 HOUR (C-2) EVERY 10,000 Flight Hours 15,000 HOUR (C-3) EVERY 15,000 Flight Hours 20,000 HOUR (C-4) EVERY 20,000 Flight Hours CALENDAR STRUCTURAL S 18 mo, 24 mo, 48 mo, 72 mo, 96 mo. Do not repeat 96 mo (one time only) 5,000 HOUR (C-1) STATUS TOTAL HOURS AT LAST 5,000 HOUR TIME REMAINING TO NEXT 5,000 HOUR PERCENT REMAINING TO NEXT 5,000 HOUR 15,025 Hours 1,654 Hours 33% 10,000 HOUR (C-2) STATUS TOTAL HOURS AT LAST 10,000 HOUR 15,025 Hours TIME REMAINING TO NEXT 10,000 HOUR PERCENT REMAINING TO NEXT 10,000 HOUR 6,654 Hours 67% 15,000 HOUR (C-3) STATUS : Adresse rcs.

3 TOTAL HOURS AT LAST 15,000 HOUR TIME REMAINING TO NEXT 15,000 HOUR PERCENT REMAINING TO NEXT 15,000 HOUR 20,000 HOUR (C-4) STATUS TOTAL HOURS AT LAST 20,000 HOUR TIME REMAINING TO NEXT 20,000 HOUR PERCENT REMAINING TO NEXT 20,000 HOUR 25,000 HOUR (C-5) STATUS TOTAL HOURS AT LAST 25,000 HOUR TIME REMAINING TO NEXT 25,000 HOUR PERCENT REMAINING TO NEXT 25,000 HOUR 12 MONTH STATUS LAST DONE NEXT DUE 11,379 Hours 8,008 Hours 53% N/A 1,629 Hours 8% N/A 6,629 Hours 27% 16-Jun Jun MONTH STATUS LAST DONE NEXT DUE 14-May May MONTH STATUS LAST DONE NEXT DUE 14-May May MONTH STATUS LAST DONE NEXT DUE 29-Apr Apr-2012 : Adresse rcs.

4 LANDING GEAR ALL DATA IS EFFECTIVE AS OF: FEBRUARY 20, 2011 POSITION Left Nose Right SERIAL NUMBER DCL 185/97 DCL 250/97 DCL 182/97 CYCLES SINCE NEW 23,074 Cycles 19,591 Cycles 23,074 Cycles OVERHAUL INTERVAL 20,000 Cycles or 10 Years, WOF 20,000 Cycles or 10 Years, WOF 20,000 Cycles or 10 Years, WOF CYCLES SINCE LAST OVERHAUL 3,025 Cycles 3,025 Cycles 3,025 Cycles DATE OF LAST OVERHAUL Feb. 20, 2009 Feb. 20, 2009 Feb. 20, 2009 CYCLES / CALENDAR TIME REMAINING TO NEXT OVERHAUL 16,975 Cycles 8 Years 16,975 Cycles 8 Years 16,975 Cycles 8 Years PERCENT REMAINING TO NEXT OVERHAUL 85% Cycles 80% Years 85% Cycles 80% Years 85% Cycles 80% Years : Adresse rcs.

5 ENGINES TYPE: GE CF34-3B1 ALL DATA IS EFFECTIVE AS OF: FEBRUARY 20, 2011 POSITION 1 2 SERIAL NUMBER TOTAL TIME 18,366 Hours 18,370 Hours TOTAL CYCLES 20,781 Cycles 20,783 Cycles TIME / CYCLES SINCE SHOP VISIT 3,348 Hours 3,025 Cycles 3,348 Hours 3,025 Cycles CYCLES TO 1 ST LIFE LIMITER 4,219 Cycles 4,217 Cycles LIMIT ITEM 7 Different LLP s See Engine Disk Life 11 Different LLP s See Engine Disk Life Note: Last Engine Boroscope Inspection accomplished March 27, 2009 on both engines. The full boroscope reports are on file in the engine records. : Adresse rcs.

6 Item ENGINE DISK LIFE ENGINE S/N ENGINE S/N Limit Remaining Limit Remaining Fan Fwd Shaft 25,000 4,219 * 25,000 4,217 * Fan Disk 24,300 4,354 24,300 16,781 Fan Drive Shaft 25,000 4,219 * 25,000 14,270 Comp Fwd Shaft 30,000 9,219 30,000 9,217 Comp Disk Stg 1 25,000 4,219 * 25,000 19,830 Comp Disk Stg 2 25,000 4,219 * 25,000 4,217 * Comp Spool Stg ,000 21,974 25,000 21,972 Comp Disk Stg 9 25,000 4,219 * 25,000 4,217 * Comp Spool Stg ,000 4,219 * 25,000 4,217 * Comp Rear Shaft 25,000 4,219 * 25,000 4,217 * CDP Seal 30,000 9,219 30,000 9,217 HPT Rotor Shaft 30,000 9,219 30,000 9,217 Bal. Piston Air Seal 18,000 14,974 18,000 14,972 Fwd Cooling Plate Stg 1 30,000 9,219 30,000 26,972 HPT Disk Stg 1 18,000 14,974 18,000 14,972 Aft Cooling Plate Stg 1 18,000 14,974 18,000 14,972 Outer Torque Coupling 30,000 9,219 30,000 9,217 Fwd Cooling Plate Stg 2 30,000 9,219 30,000 26,972 HPT Disk Stg 2 18,000 14,974 18,000 14,972 Aft Cooling Plate Stg 2 30,000 9,219 30,000 26,972 LPT Rear Shaft 25,000 5,495 25,000 4,217 * LPT Disk Stg 3 25,000 5,495 25,000 4,217 * LPT Seal Stg ,000 5,495 25,000 4,217 * LPT Disk Stg 4 25,000 21,974 25,000 21,972 : Adresse rcs.

7 ENGINE DISK LIFE Item ENGINE S/N ENGINE S/N Limit Remaining Limit Remaining LPT Seal Stg ,000 5,495 25,000 4,217 * LPT Cone Drive 25,000 5,495 25,000 4,217 * LPT Disk Stg 5 25,000 13,896 25,000 14,270 LPT Seal Stg ,000 5,495 25,000 4,217 * LPT Disk Stg 6 25,000 13,896 25,000 14,270 * Life Limiter : Adresse rcs.

8 AUXILIARY POWER UNIT (APU) MODEL NUMBER GTCP RJ SERIAL NUMBER P-682 HOURS / CYCLES SINCE NEW HOURS / CYCLES SINCE LAST SHOP VISIT (HSI PREFORMED SEPT 2008) IS APU ON CONDITION? TIME BETWEEN OVERHAUL IF APPLICABLE LIFE LIMITED (100,000 FLT HOURS or CYCLES, WOF COMPRESSOR ROTOR LIFE LIMITED (10,000 FLT HOURS or CYCLES, WOF TURBINE ROTOR 19,695 Hours 16,972 Cycles 3,185 Hours 3,260 Cycles Yes See Note Below 82,981 Hours Remaining 87,610 Cycles Remaining 6,815 Hours Remaining 6,740 Cycles Remaining Note: The manufacturer recommends that each operator preform one of the following maintenance programs for the APU: (a) Hot Section Inspection in accordance with the MRB Requirements (3,500 APU hours) OR Track and discard of APU LLP s IAW manufacturers recommended rotating component discard limits. : Adresse rcs.

9 AVIONICS LISTING Nomenclature Qty Manufacturer Part Number Auto Flight Control Computer (FCC-4000) 2 Collins Attitude Heading Computer (AHC-85E) 2 Collins EICAS (EFD-4076) 6 Collins Flight Management Computer (FMC-4200) 1 Collins Data Concentrator Unit (CDU-4000) 2 Collins IAPS Concentrator (IOC-4000) 2 Collins On-Board Data Loader 1 Collins VHF Communication Transceiver (422A) 2 Collins Digital Flight Data Recorder (FA-2100) 1 L-3 Comms Cockpit Voice Recorder (A-200S) 1 L-3 Comms S Air Data Computer (ADC-850A) 2 Collins Radio Altimeter (ALT-55) 1 Collins Radio Altimeter Converter 1 Collins Weather Radar (RTA-884) 1 Collins VHF Navigation Receiver (VIR-432) 2 Collins Automatic Direction Finder (ADF-462) 2 Collins Distance Measuring Equipment (DME-442) 2 Collins Air Traffic Control Transponder (TDR-94D) 2 Collins Collins Honeywell Traffic Alert & Collision Avoidance System (TTR- 920) Ground Proximity Warning System W/Windshear Detection (MK-V) Global Positioning System (GPS-4000) 1 Collins ELT (406 MHz) 1 Artex PA Amplifier 1 AvTech Audio Electronic Unit 1 AvTech : Adresse rcs.

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