BOMBARDIER OFFERS FOR SALE
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1 BOMBARDIER OFFERS FOR SALE CRJ900ER Serial Number TTSN 8,725 Flight Hours TCSN 9,308 Flight Cycles Page 1 of 9
2 Date of Manufacture: April, 2006 Model Designation: CL-600-2D24 Avionics MTOW - 82,500 lbs (Extended Range Version) GPS - Dual Collins Model 4000A EGPWS - Enhanced GPWS RVSM VHF Comm - Dual VHF Com FMS - DUAL Collins FMS-4200 Dual Radio Altimeter (Metric) VHF NAV - FM Immunity Single HF ELT Three Frequency, Satellite Capable. Reinforced Flight Deck Door CVR 2 Hours Interior 90 passenger seats with recline and life vest pouch dressed in gray leather G1 and FWD LAV & AFT LAV 2 nd Flight attendant seat Page 2 of 9
3 CRJ900 LOPA for Passengers Seat Pitch overwing exits) Legend: EC = Entrance Compartment; A = Attendant; G = Galley; L = Lavatory; UW = Underbin Wardrobe; US = Underbin Storage; D = = No Recline Available; T = Half-Size Trolley, S = Storage; W = Wardrobe; # = Inflatable Restraint System; I = In-Arm Table, E = Overwing Exit. B = Baggage Compartment, BD = Baggage Door, IA = Airstair Door. Baggage/Storage Capacities: 90 Passengers Total Volume Total Volume Per Pax Per Pax Total Weight Total Weight Storage Location cu.ft. cu.m cu.ft. cu.m lb. kg Aft Baggage Compt Fwd Baggage Compt Baggage Compt. Total Overhead Bins (est.) Under-seat (est.) Wardrobe (est.) Storage (est.) Dog-house (est.) Total Total Length Total Length Per Pax Per Pax Coat Rod Location in. m in. m Wardrobe (est.) Total Passenger Seats Economy: BE Silhouette Business: Status: SFE Galley Capabilities: (Space and/or Complete Provisions Provided) Equipment Type Half-Cart* Waste Half-Cart* Container* Coffee Maker* Oven* Galley Position (ATLAS Std) (ATLAS Std) (ATLAS Std) (TIA) (Tia 32 Meal) G Total * Buyer Installed Equipment Total Total Per Pax Per Pax Max Unit Weight Catering Weight lb. kg lb. kg lb. / kg Half-Cart / 64 Container 50 / 23 Galley Layout(s): Galley G1 (CR ) Page 3 of 9
4 Interior Page 4 of 9
5 G1 Galley Page 5 of 9
6 FWD Lav and CABIN Page 6 of 9
7 Flight Compartment Six Tube EFIS, Dual FMS with Dual GPS and EGPWS Page 7 of 9
8 Technical Specifications Audit Date Owner Operator Lease Del. Date Data Date Return Date 12-Feb-13 Bombardier Capital Inc (BCI) Bombardier 13-Sep Feb Aug-11 Aircraft Type MSN A/C Reg Build Date Current TSN Current CSN CRJ C-GLPP 22-Apr-06 8,725 9,308 Seats MTOW FMS HUGS IRS/AHRS ER/LR 90 82,500 lbs Collins FMS-4200 No AHRS ER Inspection Status Sytems / Powerplant / Zonal and EWIS Program BBD MRB Interval Last Done Date Flight Hours Flight Cycles Next due Remaining Interval Unit Heavy Maintenance Checks 6,000 40,311 6,996 8,077 12, ,271 HRS 12,000 12, ,275 HRS Structures / CPCP / SSI Program 72 Month Initial (6 YR Check) 2, Apr Apr DAYS 96 Month/72 Month Repeat (8 YR / 6 YR Repeat) Dec-05 DAYS 144 Month/108 Month Repeat (12 YR / 9 YR Repeat) 3, Dec-08 DAYS Left Engine Type: 8C1 or 8C5 Serial Number TTSN TCSN TSLSV CSLSV CF34-8C5 GE-E ,686 9,363 1,721 1,229 LLP's Description Part Number Serial No Cycles Since New Cycles Remaining Cycle Life Limit Fan Rotor Assembly Disk, Fan 4114T16G02 IHI203AB 9,363 15,637 25,000 Shaft, Fan Drive 4118T61P01 IHI498DW 9,363 15,637 25,000 Compressor Rotor Assembly Blisk, Compressor Rotor, Stage 1 and T60P01 GLHTJAFA 9,363 15,637 25,000 Shaft, HP Compressor Forward 4128T91G05 TMTYW265 9,363 15,637 25,000 Blisk, Compressor Rotor Stage T59P02 GLHTJCDN 9,363 15,637 25,000 Spoiler, High Pressure Compressor Rotor Vortex 4129T40P01 BJWF5491 9,363 15,637 25,000 Spool, Compressor Rotor Aft Shaft 4129T50G03 GWN0C7H9 9,363 15,637 25,000 Seal, Compressor Discharge 4129T28P05 XAE ,363 15,637 25,000 HPT Rotor Assembly Air Seal, Inner Balance Piston Rotating 4124T93P03 FDU4555A 9,363 15,637 25,000 Air Seal, High Pressure Turbine Outer Balance Piston Rotating 4124T92P02 FDU5500A 9,363 15,637 25,000 Cooling Plate, Stage 1 High Pressure Turbine Forward 4125T30P01 NCE 004BD 9,363 15,637 25,000 Disk, Stage 1 Turbine Rotor 4125T22P03 GATHH00R 9,363 14,837 24,200 Coupling, High Pressure Turbine Outer Torque 4125T37P02 TMTUD900 1,229 23,771 25,000 Disk, Stage 2 Turbine Rotor 4125T23P04 GATHH1D4 9,363 15,637 25,000 Cooling Plate, Stage 2 High Pressure Turbine Aft 4124T95P03 NCE429BC 9,363 15,637 25,000 LPT Rotor Assembly Disk, Stage 3 LPT 4118T63P01 IHI192VF 9,363 15,637 25,000 Seal, Stages 3 and 4 Turbine 4117T16P01 WES515CK 9,363 15,637 25,000 Disk, Stage 4 LPT 4117T13P04 IHI192VL 9,363 15,637 25,000 Seal, Stages 4 and 5 Turbine 4117T17P01 WES494CR 9,363 15,637 25,000 Shaft, Rear LPT 4118T62P01 IHI165WF 9,363 15,637 25,000 Disk, Stage 5 LPT 4117T14P02 IHI181VT 9,363 15,637 25,000 Seal, Stages 5 and 6 Turbine 4117T18P01 WES424CY 9,363 15,637 25,000 Disk, Stage 6 LPT 4117T15P02 IHI764BA 9,363 15,637 25,000 Static Structures Front Frame and Bearing Support Assembly 4145T54G14 PAMFF873 9,363 70,637 80,000 Combustion Chamber Assembly 4180T27G04 GEVKRPAL 9,363 31,737 41,100 Fan OGV Frame 4126T00G12 TRIBA565 9, , ,000 Engine Rear Mount Link 4126T40G01 SAM1455C 9, , ,000 Engine Mount Link Assembly 4126T42G01 FEKL0066 9, , ,000 Front Frame Yoke 4138T20G01 SAM1382B 9,363 70,637 80,000 Forward Mount Clevis (1) 4126T12G04 FDU3860A 9, , ,000 Forward Mount Clevis (2) 4126T12G04 FEK370AA 9, , ,000 Case, Compressor 1822M28G02 CDAC6463 9,363 19,037 28,400 Mount - Rear, Engine 4131T97G01 CDAAA599 9, , ,000 Ring - Rear, Main Mount 4131T18G01 SAM4421D 9, , ,000 Bolt - Double Hex Shoulder 4126T47P02 SNAN0160 9, , ,000 Bolt - Double Hex Shoulder (1) 4126T92P02 SNAP0607 9, , ,000 Bolt - Double Hex Shoulder (2) 4126T92P02 SNAP0906 9, , ,000 Bolt -Square Head Shoulder (1) 4126T93P02 SNAR0601 9, , ,000 Bolt -Square Head Shoulder (2) 4126T93P02 SNAR0625 9, , ,000 specified "Data Date." While diligent efforts have been made by Bombardier to verify such specifications to the extent possible, Bombardier shall not be held responsible for any inaccurate data supplied by the previous operator. Prospective customers are strongly encouraged to Page 8 of 9
9 Right Engine Type: 8C1 or 8C5 Serial Number TTSN TCSN TSLSV CSLSV CF34-8C5 GE-E ,686 9,363 1,721 1,229 LLP's Description Part Number Serial No Cycles Since New Cycles Remaining Cycle Life Limit Fan Rotor Assembly Disk, Fan 4114T16G02 IHI174AB 9,363 15,637 25,000 Shaft, Fan Drive 4118T61P01 IHI519DW 9,363 15,637 25,000 Compressor Rotor Assembly Blisk, Compressor Rotor, Stage 1 and T60P01 GLHTJAFC 9,363 15,637 25,000 Shaft, HP Compressor Forward 4128T91G05 TMTYW233 9,363 15,637 25,000 Blisk, Compressor Rotor Stage T59P02 GLHTJAGC 9,363 15,637 25,000 Spoiler, High Pressure Compressor Rotor Vortex 4129T40P01 BJWF5489 9,363 15,637 25,000 Spool, Compressor Rotor Aft Shaft 4129T50G03 GWN0C7TR 9,363 15,637 25,000 Seal, Compressor Discharge 4129T28P05 XAE ,363 15,637 25,000 HPT Rotor Assembly Air Seal, Inner Balance Piston Rotating 4124T93P03 XAEE5045 9,363 15,637 25,000 Air Seal, High Pressure Turbine Outer Balance Piston Rotating 4124T92P02 FDU4916A 9,363 15,637 25,000 Cooling Plate, Stage 1 High Pressure Turbine Forward 4125T30P01 NCE023BD 9,363 15,637 25,000 Disk, Stage 1 Turbine Rotor 4125T22P03 GATHH01A 9,363 14,837 24,200 Coupling, High Pressure Turbine Outer Torque 4125T37P02 XAE ,363 15,637 25,000 Disk, Stage 2 Turbine Rotor 4125T23P04 GATHGWJW 9,363 15,637 25,000 Cooling Plate, Stage 2 High Pressure Turbine Aft 4124T95P03 NCE424BC 9,363 15,637 25,000 LPT Rotor Assembly Disk, Stage 3 LPT 4118T63P01 IHI800AF 9,363 15,637 25,000 Seal, Stages 3 and 4 Turbine 4117T16P01 WES510CK 9,363 15,637 25,000 Disk, Stage 4 LPT 4117T13P04 IHI178VL 9,363 15,637 25,000 Seal, Stages 4 and 5 Turbine 4117T17P01 WES482CR 9,363 15,637 25,000 Shaft, Rear LPT 4118T62P01 IHI129WF 9,363 15,637 25,000 Disk, Stage 5 LPT 4117T14P02 IHI197VT 9,363 15,637 25,000 Seal, Stages 5 and 6 Turbine 4117T18P01 WES444CY 9,363 15,637 25,000 Disk, Stage 6 LPT 4117T15P02 IHI760BA 9,363 15,637 25,000 Static Structures Front Frame and Bearing Support Assembly 4145T54G14 PAMFG495 9,363 70,637 80,000 Combustion Chamber Assembly 4180T27G04 GEVKRMWL 9,363 31,737 41,100 Fan OGV Frame 4126T00G12 FEKM0025 9, , ,000 Engine Rear Mount Link 4126T40G01 SAM1425C 9, , ,000 Engine Mount Link Assembly 4126T42G01 WAGW0592 9, , ,000 Front Frame Yoke 4138T20G01 SAM1313B 9,363 70,637 80,000 Forward Mount Clevis (1) 4126T12G04 FDU4513A 9, , ,000 Forward Mount Clevis (2) 4126T12G04 FDU4522A 9, , ,000 Case, Compressor 1822M28G02 CDAC6497 9,363 19,037 28,400 Mount - Rear, Engine 4131T97G01 CDAAE771 9, , ,000 Ring - Rear, Main Mount 4131T18G01 SAM4311D 9, , ,000 Bolt - Double Hex Shoulder 4126T47P02 SNAN0206 9, , ,000 Bolt - Double Hex Shoulder (1) 4126T92P02 SNAP0753 9, , ,000 Bolt - Double Hex Shoulder (2) 4126T92P02 SNAP0593 9, , ,000 Bolt -Square Head Shoulder (1) 4126T93P02 SNAR0607 9, , ,000 Bolt -Square Head Shoulder (2) 4126T93P02 SNAR0560 9, , ,000 Landing Gear Description Installed Cycles Part Number Serial No Since New Since Restoration NOSE GEAR Nose Landing Gear Assy MA1117 6,225 Not Due Yet MAIN GEAR, LEFT Main Landing Gear Assy MA1129 6,225 Not Due Yet MAIN GEAR, RIGHT Main Landing Gear Assy MA1130 6,225 Not Due Yet APU APU Model Part Number Serial Number CSN CSO TSN TSO D.O.M. Date of Inst RE220 (RJ) WE P ,862 11,862 9,846 9, Jan-06 8-Feb-06 LLP Description Part Number Serial Number CSN CSO TSN TSO Limit Remaining Compressor (Impeller) WB ,862 11,862 9,846 9,846 17,000 5,138 1st Stage Turbine Rotor WK ,862 11,862 9,846 9,846 17,000 5,138 2nd Stage Turbine Rotor WE ,862 11,862 9,846 9,846 17,000 5,138 specified "Data Date." While diligent efforts have been made by Bombardier to verify such specifications to the extent possible, Bombardier shall not be held responsible for any inaccurate data supplied by the previous operator. Prospective customers are strongly encouraged to Page 9 of 9
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