Specifications
A330-200 | A330-200F | A330-300 | ||
---|---|---|---|---|
Cockpit crew | Two | |||
Seating capacity, typical |
253 (3-class) 293 (2-class) 380 (maximum) |
n/a | 295 (3-class) 335 (2-class) 440 (maximum) |
|
Length | 58.82 m (193 ft 0 in) | 63.69 m (208 ft 11 in) | ||
Wingspan | 60.3 m (197 ft 10 in) | |||
Wing area | 361.6 m2 (3,892 sq ft) | |||
Aspect Ratio | 10.06 | |||
Wing sweepback | 30° | |||
Tail height | 17.39 m (57 ft 1 in) | 16.90 m (55 ft 5 in) | 16.83 m (55 ft 3 in) | |
Cabin width | 5.28 m (17 ft 4 in) | |||
Fuselage width | 5.64 m (18 ft 6 in) | |||
Cargo capacity | 136 m3 (4,800 cu ft) | 475 m3 (16,800 cu ft) 70 t / up to 12 couriers |
162.8 m3 (5,750 cu ft) | |
Operating empty weight (typical) |
119,600 kg (264,000 lb) | 109,000 kg (240,000 lb) | 124,500 kg (274,000 lb) | |
Maximum Takeoff Weight (MTOW) |
233,000 kg (510,000 lb) to 238,000 kg (520,000 lb) |
227,000 kg (500,000 lb) to 233,000 kg (510,000 lb) |
230,000 kg (510,000 lb) to 235,000 kg (520,000 lb) |
|
Maximum Landing Weight | 180,000 kg (396,900 lb) | 185,000 kg (407,925 lb) | ||
Cruise speed | Mach 0.82 (871 km/h, 470 kn; 541 mph at 11,000 m/36,000 ft cruise altitude) | |||
Maximum cruise speed | Mach 0.86 (913 km/h, 493 kn; 567 mph at 11,000 m/36,000 ft cruise altitude) | |||
Maximum range, fully loaded | 13,430 km (7,250 nmi) | 7,400 km (4,000 nmi) | 10,830 km (5,850 nmi) | |
Maximum range, fully fuelled | 14,390 km (7,770 nmi) | 7,930 km (4,280 nmi) | 12,040 km (6,500 nmi) | |
Takeoff distance at MTOW | 2,220 m (7,280 ft) | n/a | 2,500 m (8,200 ft) | |
Maximum fuel capacity | 139,090 L (36,740 US gal) | 97,530 L (25,760 US gal) | ||
Service ceiling | 12,527 m (41,100 ft) | |||
Maximum service ceiling | 13,000 m (42,651 ft) | |||
Engines (×2) |
General Electric CF6-80E1 Pratt & Whitney PW4000 Rolls-Royce Trent 700 |
Pratt & Whitney PW4000 Rolls-Royce Trent 700 |
General Electric CF6-80E1 Pratt & Whitney PW4000 Rolls-Royce Trent 700 |
|
Thrust (×2) | PW: 70,000 lbf (311 kN) RR: 71,100 lbf (316 kN) GE: 72,000 lbf (320 kN) |
PW: 70,000 lbf (311 kN) RR: 71,100 lbf (316 kN) |
PW: 70,000 lbf (311 kN) RR: 71,100 lbf (316 kN) GE: 72,000 lbf (320 kN) |
Sources: Airbus, Pratt & Whitney, EASA, FAA, The International Directory of Civil Aircraft
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