1980 BOEING 747 SP

1980

BOEING

747-SP

Used

46076.0

7820FC Total Cycles Weights: Maxi Taxi Weight: 703,000 lbs (318, 875 kg) Maxi Take-Off weight: 696,000 lbs (315,700 kg) Maxi Landing weight: 450,000 lbs (204,116 kg) Maxi Zero Fuel Weight: 410,000 lbs (185,972 kg) Landing Gears: TBO: 10 years Nose LDG: Overhaul due Feb 2009 Main LDG: Overhaul due Jun 2011

Pratt & Whitney JT9D-7 Position S/N Type Install. Date TSN CSN TSO CSO 1 662 802 -7A 07-May-04 63,312 15,512 1,716 758 2 662 685 -7J 01-May-97 45,797 12,418 2,038 963 3 695 748 -7J 01-May-03 42,182 10,490 2,444 1,137 4 695 788 -7A 11-Apr-02 50,611 7,540 1,896 889 APU: (currently in shop) Make: Garrett Model: GTCP660-4 Serial Number: 37,749 Total Hours: 38,675 Hours Since Overhaul: 2,240

Equipment Vendor Model Qty Autopilot Sperry SP1 2 TCAS II Honeywell RT910 1 ELT CEIS 06UZ 1 VHF Comm. TX/RX Collins 618M-3 3 HF Comm. TX/RX Collins 627T-1 2 Executive Comm. System Racal Satphone UNK 1 VOR/ILS RX Collins 51RV-2 3 Marker RX Collins 51Z-4 1 ADF RX Collins 51Y-7 2 DME TX/RX Collins 860E-5 2 ATC Transponder Honeywell Mode S 2 Radio Altimeter Collins 860F-1 3 Inertial Navigation System Delco Carousel IV 3 Weather Radar TX/TX RCA Primus 90 2 Digital Fuel Indication System BF Goodrich The aircraft is RVSM approved, radio com/nav equipment are FM immune, VHF 8.33 kHz channel spacing.

VIP Configuration. Total number of seats: 125 or 135 (depending on staff seating arrangement) 6 Sections: Lounge (10 seats: 6 chairs & 2 double sofas) Bedroom/Bathroom (1 chair) VIP Seating (18 First Class Seats) Business Class seating (40 Business Class Seats) Staff seating (44 or 54 Business Class Seats) Upper deck (12 First Class Seats)

Low Utilization Program Check Interval Last Done Next Due C 2 years or 1000 FH May 03 May 05 (C) C2 (*) 6 years or 3000 FH May 03 May 05 (3C2) C3 8 years or 9000 FH Jun 01 Jun 09 (C3) C4 12 years or 12000 FH Apr 93 May 05 (C4) C6/7 (**) 12 years or 18000 FH Jun 01 May 05 (3C6/7) Structural (***) 18 years or 18000 FH Apr 93 Apr 07 1/3 * Check completed in 3 successive phases, one phase to be completed bi-annually or every 1000 FH (C2=1C2 + 2C2 + 3C2) ** Check completed in 3 successive phases, one phase to be completed every 4 years (C6/7= 1C6/7 + 2C6/7 + 3C6/7) *** Inspection completed in 3 successive phases (wings, tail and fuselage), one phase to be completed in each of the 14th, 16th and 17th years