On Oct 29, 2010
SPECS
| Cockpit crew | : Two | |||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Passengers | : | 218 (3 class), 269 (2 class), 350 (1 class) | ||||||||||
| Cargo | : | 3,770 ft³ (106.8 m³) 30 LD2s | ||||||||||
| Length | : | 180 ft 3 in (54.9 m) | ||||||||||
| Wingspan | : 156 ft 1 in (47.6 m) | |||||||||||
| Wing area | : 3,050 ft² (283.3 m²) | |||||||||||
| Fuselage height | : 17 ft 9 in (5.41 m) | |||||||||||
| Fuselage width | : 16 ft 6 in (5.03 m) | |||||||||||
| Cabin width (interior) | : 15 ft 6 in (4.72 m) | |||||||||||
| Maximum Fuel Capacity | : 23,980 U.S. gal (90,770 L) | |||||||||||
| Empty Weight, operating | : | 189,750 lb (86,070 kg) | ||||||||||
| Maximum take-off weight | : | 350,000 lb (158,760 kg) | ||||||||||
| Maximum Range at MTOW | : | 3,950 nmi(7,300 km) transatlantic | ||||||||||
| Cruise speed: | Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft cruise altitude) | |||||||||||
| Max. Cruise speed: | Mach 0.86 (493 knots, 568 mph, 913 km/h at 35,000 ft cruise altitude) | |||||||||||
| Takeoff run at MTOW: | 7,900 ft (2,410 m) | |||||||||||
| Engines (x2): | P&W JT9D-7R4,P&W PW4000-94,GE CF6-80A,GE CF6-80C2 | |||||||||||
| Thrust (x2): | PW: 50,000 lbf (220 kN) | |||||||||||