1999 BOEING 777 200

1999

BOEING

777-200

Used

IFR

Four (4) 1999 Boeing 777-200ER aircrafts with the same configurations available for immediate delivery. 380 Passenger Configuration. For additional information please call. 1999 Boeing 777-200ER

336685.0

AIRFRAME Effective date: APR 30,2008 Aircraft type: B777-200ER Date of manufacture: 1999.12.28 Total Airframe hours since new: 33668:50 Total Airframe cycles since new: 14851 ___________________________________________________________ LANDING GEARS: MLG LH MLG RH NLG Part number: 161W1000-7 161W1000-8 162W1000-5 Total time since new: 37050 37050 37050 Total cycles since new: 9602 9602 9602 Time since overhaul: 7393 7393 7393 Cycles since overhaul: 2979 2979 2979 Time between overhaul: 10000~16000Fc 10000~16000Fc 10000~16000Fc 10Yr 10Yr 10Yr Last overhaul date:OCT.2005 OCT.2005 OCT.2005

ENGINES Engine 1 Engine 2 APU Type/Model: GE90-90B GE90-90B 3800550-1 Thrust rating: 90000 lbs 90000 lbs Effective date: APR30,2008 APR30,2008 APR30,2008 Time Since New: 29053:13 30720:46 17539 Cycles Since New:9522 10637 15313 Time Since Last Shopvisit:2617:40 6001:35 950 Cycles Since Last Shopvisit: 431 1436 933 Cycles remaining first limiter 1748 3560 11687 First limiter description:SEAL INTERSTAGE DISKCSTG 1 HPTR

29053

SNEW

30720

SNEW

Major Avionic Equipment ATA Part Number Description QTY Manufacturer 22 822-0006-103 AFDC 3 ROCKWELL 23 622-8971-522 TCAS 1 ROCKWELL 23 822-0330-001 HF RADIO SYS 2 ROCKWELL 23 822-1047-003 VHF COMM UNIT 3 ROCKWELL 23 5700-1-7 AUDIO MANAGEMENT 1 AVTECH 23 980-6020-001 VOICE RECORDER 1 ALLIEDSIGNAL 23 980-6117-004 COCKPIT VOICE RECORDER 1 ALLIEDSIGNAL 23 SC2253AD01 SEL-CAL DECODER 1 TEAM 34 822-0297-001 VOR RECEIVER 2 ROCKWELL 34 822-0298-001 ILS 3 ROCKWELL 34 822-0299-001 ADF RECEIVER 2 ROCKWELL 34 822-0329-001 DME 2 ROCKWELL 34 822-0334-002 RADIO ALTIMETER 3 ROCKWELL 34 622-8973-001 TCAS ANTENNA 2 ROCKWELL 34 822-1338-003 ATC TRANSPONDER 2 ROCKWELL 34 2041217-0418 WEATHER RADAR 1 ALLIEDSIGNAL

Additional Equipment: ATA Description Qty Manufacturer Part number 25-24 Forward Coat Closet RH/LH 2/2 BOEING 25-24 Centre Coat Closet RH/LH 1/1 BOEING 25-25 First Class double seat-LH 2 Koito 83-222B7451-403 25-25 First Class double seat-RH 2 Koito 83-222B7451-404 25-25 Economy Class triple seat-LH 10 Sicma 9501310-11 25-25 Economy Class triple seat-RH 8 Sicma 9501300-02 25-25 Economy Class double seat-LH 2 Sicma 9501210-25 25-25 Economy Class double seat-RH 2 Sicma 9501200-26 25-31 Galley F1 1 CFTaylor M5949-1 25-31 Galley F2 1 CFTaylor M5552-1 25-31 Galley F3 1 CFTaylor M5553-1 25-31 Galley M1 1 CFTaylor M5562-1 25-32 Container full size 41 Lermer GMBH L20737-11 25-32 Oven 17 B/E 25-32 Coffeemaker 4 A/C PRODUCT 3510-0044-05 25-32 Water boiler 5 L A Rumbold HE62190

2008

White

1999

380

Interior Configuration Passenger compartment: 2-Class configuration. 24 First Class Seats at 38" pitch and 356 Economy Class Seats at 32h pitch. All seats are covered with fabric covers. All seats are equipped with life vests installed under seats. Cabin is fitted with floor mounted escape path lighting. 16 Attendant seats installed (5 fwd cabin, 4 mid section, 2 mid section, 5 aft section). 10 Lavatories installed (2-fwd cabin, 2-fwd mid cabin, 4-mid cabin,2 aft cabin). 9 Galley installed (F-1, F-2, F-3, F-5 in fwd cabin, M-1,M-2 in Mid cabin, A-1, A-2, A-3 - Aft cabin).

OPERATIONAL WEIGHTS Date last weighing: JUL 05,2007 Maximum Taxi Weight: 248,115 Kgs 547,000 Lbs Maximum Take-off Weight: 247,207 Kgs 545,000 Lbs Maximum Landing Weight: 201,848 Kgs 445,000 Lbs Maximum Zero Fuel Weight:190,508 Kgs 420,000 Lbs Basic Empty Weight: 134,511 Kgs 296,598 Lbs Operating Empty Weight: 139,466 Kgs 307,522 Lbs FUEL Fuel Quantity Indication units: KGsX1000 Fuel Flow Indication units: KGS/HrX1000 Total Fuel Capacity: 95,045 Kgs, 209,560 Lbs, 31,000 USg Capacity Center Wing Tank:38,021 Kgs,83,824 Lbs, 12,400 USg Capacity Main Wing Tank :28,512 Kgs,62,868 Lbs, 9,300 USg

Maintenance Transit Check performed every Maintenance Base visit. Daily Check performed each day not to exceed 48 hours. A-check performed each 600 FH or 400 FC or 90 Days (whichever comes first) and numbered from 1 thru 120. A-check performed each 300 FH or 200 FC or 45 Days (whichever comes first) and numbered from 1 thru 240. C-check includes the system and structure C-check. C-check performed each 7500 FH for systems C-check MPD tasks. C-check performed 4000 FC or 750 Days (whichever comes first) for structure C-check MPD tasks. Maintenance history Date Hours Cycles Location C-checkSTR C6+SYS C6 2007-6-3 30915-13848 GAMECO Guangzhou