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1 Offers for Sale or Lease CRJ200LR Serial Number 7391 TTSN 25,589 Flight Hours TCSN 21,550 Flight Cycles Page 1 of 10

2 Date of Manufacture: April, 2000 Model Designation: CL-600-2B19 Avionics Collins Proline 4 Avionics Suite Re-inforced Cockpit Door EICAS 2000 Update Dual Collins FMS-4200 Long Range- 53,000 lbs MTOW Dual IRS CVR- 2 Hours, Solid State VHF COMM - Dual, 8.33 khz Channel spacing HF Radio HGS - CAT IIIA FULL INSTALLATION Dual Collins GPS Altimeter- Metric Indication Dual Radio Altimeter 3 Frequency ELT - Artex Interior 50 Passenger Configuration G1 Galley with two (2) ovens and one (1) Coffee Maker G2 Galley with Snack Service 2 nd Flight Attendant Seat Centre-Entry Lavatory Page 2 of 10

3 GALLEY LAVAT ORY ON W ON CONTRO L F F A OF F OF F T E L PUMP R PUMP A PUMP PUMP G POWE R OUTLET V A L A E T L ON V ON O TANK TANK E E R HE AT ER HEATER E E Y OF F L OF F Y LEFT RI GH FREEZ E FREEZ E LIN E LI N E PROTECTION PROTECTION HEAT ERS HE AT ERS T CRJ200 LOPA for UTAir 50 Passengers Seat Pitch overwing exit) G1 G L A A EC 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 Required; I = With In-Arm Table. Baggage/Storage Capacities: 50 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 Overhead Bins (est.) Under-seat (est.) Wardrobe (est.) Storage (est.) Total Total Length Total Length Per Pax Per Pax Coat Rod Location in. m in. m Wardrobe (est.) Total Galley Capabilities: (Space and/or Complete Provisions Provided) Equipment Type Half-Cart Waste Cart Container Coffee Maker Oven Galley Position (ATLAS Std) (ATLAS Std) (ATLAS Std) (TIA 1448) (Tia meal) G G2 2 5 Total Total Total Per Pax Per Pax Max Unit Weight Catering Weight lb. kg lb. kg lb. / kg Half-Cart / 64 Container / 23 Total Galley Layout(s): Passenger Seats Economy: BE Silhouette Business: Status: SFE E X I Galley G1 Galley G2 Page 3 of 10

4 Interior Page 4 of 10

5 G1 Galley Page 5 of 10

6 G2 Galley Page 6 of 10

7 Flight Compartment Six Tube EFIS, Dual FMS Page 7 of 10

8 Technical Specifications Data Date Owner Operator Factory Deliv. Delivery Date Audit Date Jurisdiction 13-Jun-13 Bombardier Inc. UTair Aviation 15-May Oct Jun-13 TC/FAA Aircraft Type A/C Serial No A/C Reg Build Date Current TSN Current CSN Date: Remain Forecast CRJ VQ-BGW 26-Apr-00 25,589 21, Jun-13 Airframe Configuration Seats MTOW FMS IRS/AHRS HUGS ER/LR 50 53,000 Dual FMS Dual IRS Yes LR Inspection Status Last Done Check Description Interval (MRB) Date Flight Hours Flight Cycles Next due Remain (MRB) Interval Unit Repair Station 5,000 9-Aug-10 21,524 19,263 26, FH LHT, Cologne 10,000 9-Aug-10 21,524 19,263 31,524 5,935 FH LHT, Cologne Heavy Maintenance Checks 15,000 9-Aug-10 21,524 19,263 36,524 10,935 FH LHT, Cologne 20, Sep-08 18,720 16,539 38,720 13,131 FH LHT, Cologne 25, Sep-08 18,720 16,539 43,720 18,131 FH LHT, Cologne 30,000 9-Aug-10 21,524 19,263 51,524 25,935 FH LHT, Cologne 24 M C Jan-13 25,048 21, Jan Days SIBIR TECHNICS FC Structural 40,000 0-Jan ,000 18,450 FC 0 48M- (4yr)SIP 1, Jan-13 25,048 21, Jan Days SIBIR TECHNICS 72M- (6yr)SIP 2,192 9-Aug-10 21,524 19,263 9-Aug Days LHT, Cologne 48/ Jan-13 25,048 21, Jan Days RUSLINE, Vnukovo 72/48 1, Jan-13 25,048 21, Jan Days SIBIR TECHNICS 96/48 1,461 9-Aug-10 21,524 19,263 9-Aug Days LHT, Cologne 96/72 2, Jan-13 25,048 21, Jan Days SIBIR TECHNICS Left Engine Type Serial Number TTSN TCSN TSLSV CSLSV CF34-3B C 31,925 26,719 14,626 12,455 Shop Visit History HSI or O/H TSN CSN Agency REPAIR & CONV. TO 3B1 ( ) 17,299 14,264 LUFTHANSA AERO LLP's Description Part Number Serial No Cycles Since New Cycles Remaining Cycle Life Limit Fan Rotor Assembly Disk, Fan 6078T57G05 GEE142V6 19,615 4,685 24,300 Shaft, Forward Fan 6078T51P02 GAT9647R 21,873 3,127 25,000 Shaft, Fan Drive 6036T78P02 REA1762H 21,948 3,052 25,000 Compressor Rotor Assembly Blisk, Stage 1 Compressor Rotor 5087T84P01 GLHTH1NG 12,455 9,745 22,200 Shaft, Compressor Forward 5037T01P04 PAMEB763 12,455 17,545 30,000 Disk, Stage 2 Compressor Rotor 6036T91P02 GATHECAW 12,455 12,545 25,000 Spool, Stage 3-8 Compressor Rotor 6078T56P05 GWN08GM6 12,455 12,545 25,000 Disk, Stage 9 Compressor Rotor 6087T01P03 HAAK ,455 12,545 25,000 Shaft, Compressor Rotor Rear 6087T03P03 GWN088TH 12,455 12,545 25,000 Seal, Compressor Discharge Rotating 4019T38P01 PAMBJ467 12,455 17,545 30,000 Spool, Stage Compressor Rotor 5087T46P02 GWN08KG1 12,455 12,545 25,000 HPT Rotor Assembly Seal, Balance Piston Air 5079T63P02 NCE4910W 12,455 5,545 18,000 Shaft, HPT Rotor 5079T62P02 GEE ,071 8,929 30,000 Plate, Stage 1 Front Cooling 5079T65P06 NCE2714F 26,719 3,281 30,000 Disk, Stage 1 Turbine 5079T52P09 GATHECG1 12,455 5,545 18,000 Plate, Stage 1 Aft Cooling 5123T02P01 NCE9110W 12,455 5,545 18,000 Coupling, Outer Torque 5079T64P05 GATHCRVR8 26,719 3,281 30,000 Plate, Stage 2 Front Cooling 5079T55P04 NCE8249W 12,455 17,545 30,000 Disk, Stage 2 Turbine 5079T73P04 GATHEAD1 12,455 5,545 18,000 Plate, Stage 2 Rear Cooling 5079T56P02 NCE3285M 12,455 17,545 30,000 LPT Rotor Assembly Shaft, Turbine Rear 6030T72P02 NCE5745W 6,960 18,040 25,000 Disk, Stage 3 Turbine 6078T91P01 GATBFH34 5,161 19,839 25,000 Seal, Stage 3 and 4 Turbine 5023T59P02 WES ,011 19,989 25,000 Disk, Stage 4 Turbine 6078T02P03 GATHDPDK 7,807 17,193 25,000 Seal, Stage 4 and 5 Turbine 5023T67P01 WES ,454 12,546 25,000 Cone, Turbine Drive 5023T40P03 NCE6237Y 5,030 19,970 25,000 Disk Stage 5 Turbine 6078T92P01 GATHDJP8 12,354 12,646 25,000 Seal, Stage 5 and 6 Turbine 5023T64P02 WES ,354 12,646 25,000 Disk, Stage 6 Turbine 6078T89P03 GATHDE8W 12,354 12,646 25,000 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 10

9 Right Engine (Note: This engine is not original to this aircraft and is a LOANER, therefore NO DATA is represented, the original engine is in the shop. The original ESN is in repair at Iberia awaiting further instructions from UTAIR. Type Serial Number TTSN TCSN TSLSV CSLSV CF34-3B C Shop Visit History HSI or O/H TSN CSN Agency LLP's Description Part Number Serial No Cycles Since New Cycles Remaining Cycle Life Limit Fan Rotor Assembly Disk, Fan Shaft, Forward Fan Shaft, Fan Drive Compressor Rotor Assembly Blisk, Stage 1 Compressor Rotor Shaft, Compressor Forward Disk, Stage 2 Compressor Rotor Spool, Stage 3-8 Compressor Rotor Disk, Stage 9 Compressor Rotor Shaft, Compressor Rotor Rear Seal, Compressor Discharge Rotating Spool, Stage Compressor Rotor HPT Rotor Assembly Seal, Balance Piston Air Shaft, HPT Rotor Plate, Stage 1 Front Cooling Disk, Stage 1 Turbine Plate, Stage 1 Aft Cooling Coupling, Outer Torque Plate, Stage 2 Front Cooling Disk, Stage 2 Turbine Plate, Stage 2 Rear Cooling LPT Rotor Assembly Shaft, Turbine Rear Disk, Stage 3 Turbine Seal, Stage 3 and 4 Turbine Disk, Stage 4 Turbine Seal, Stage 4 and 5 Turbine Cone, Turbine Drive Disk Stage 5 Turbine Seal, Stage 5 and 6 Turbine Disk, Stage 6 Turbine Landing Gear Description Installed Cycles Date Part Number Serial No Since New Since Restoration Last Restored Nose Gear NLG Assy N/A 20,271 2, Nov-09 Main Gear, Left MLG Assy MDT1148 N/A 2, Mar-07 Main Gear, Right MLG Assy DCL N/A 9,160 6-Jul-07 APU Total Hours Total Cycles Description Part Number Serial No Since New Since H.S.I Since New Since Repair APU Assy GTCP RJ P-253C 23, , Compressor Wheel (Impeller) , ,765 0 Turbine Wheel 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 10

10 UPDATED DATA for ENGINE LLPs as at April 10, 2014 MSN 7391 Total Airframe Flight Hours : 26,924 Total Airframe Flight Cycles : 22,301 Engine Life Limited Parts ESN C ESN CSN : 27,470 CSN : 20,124 Cycles Remaining Cycles Remaining Fan Rotor Assembly Disk, Fan 2,530 24,800 Shaft, Forward Fan 2,376 24,800 Shaft, Fan Drive 2,301 24,800 Compressor Rotor Assembly Blisk, Stage 1 Compressor Rotor 2,301 2,076 Shaft, Compressor Forward 16,974 9,876 Disk, Stage 2 Compressor Rotor 4,794 4,876 Spool, Stage 3-8 Compressor Rotor 11,794 1,876 Disk, Stage 9 Compressor Rotor 11,794 4,876 Shaft, Compressor Rotor Rear 11,794 4,876 Seal, Compressor Discharge Rotating 16,794 2,481 Spool, Stage Compressor Rotor 11,794 4,876 HPT Rotor Assembly Seal, Balance Piston Air 4,794 2,481 Shaft, HPT Rotor 8,178 13,639 Plate, Stage 1 Front Cooling 2,530 13,629 Disk, Stage 1 Turbine 3,934 17,139 Plate, Stage 1 Aft Cooling 4,794 2,567 Coupling, Outer Torque 19,219 13,639 Plate, Stage 2 Front Cooling 16,794 13,639 Disk, Stage 2 Turbine 11,974 5,749 Plate, Stage 2 Rear Cooling 16,794 13,639 LPT Rotor Assembly Shaft, Turbine Rear 17,289 13,971 Disk, Stage 3 Turbine 19,088 13,971 Seal, Stage 3 and 4 Turbine 19,238 11,921 Disk, Stage 4 Turbine 16,442 11,921 Seal, Stage 4 and 5 Turbine 11,795 11,921 Cone, Turbine Drive 8,994 13,971 Disk Stage 5 Turbine 11,895 13,971 Seal, Stage 5 and 6 Turbine 11,895 11,921 Disk, Stage 6 Turbine 4,794 13,971 The equipment specifications set forth herein are based on information provided by the last operator of the aircraft, and are current as at the specified "Data Date April 10, 2014." 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 inspect the equipment and review the related maintenance records. Page 10 of 10

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