Technical Data Airbus A330-200F
Aircraft Dimensions
| ft | m | |
| Overall length | 192ft 1in | 58.8 |
| Height | 55ft 5in | 16.90 |
| Fuselage diameter | 18ft 6in | 5.64 |
| Maximum cabin width | 17ft 4in | 5.28 |
| Cabin length | 133ft 1in | 40.8 |
| Wing span (geometric) | 197ft 10in | 60.3 |
| Wing area (reference) | 3 892ft2 | 361.6 m2 |
| Wing sweep (25% chord) | 30 degrees | 30 degrees |
| Wheelbase | 72ft 10in | 22.2 |
| Wheel track | 35ft 1in | 10.69 |
Basic Operation Data
| imperial | metric | |
| Engines |
2 x CF6-80E1 or PW4000 or RR Trent 700 |
2 x CF6-80E1 or PW4000 or RR Trent 700 |
| Engine thrust range | 68 000-72 000 lb. slst | 303-320 kN |
| Typical passenger seating | NA | NA |
| Range (max. pax) | 4 000 nm | 7,400 km |
| Max. operating Mach number (Mmo) | 0.86 Mo. | 0.86 Mo. |
| Bulk hold volume - Standard/option | 695.7 / 486 ft3 | 19.7 / 13.76 m3 |
Design Weights
| imperial | metric | |
| Max. ramp weight | 515.7 (502.4) lbs. x 1000 | 233.9 (227.9) t |
| Max. take-off weight | 513.7 (500.4) lbs. x 1000 | 233 (227) t |
| Max. landing weight | 401.2 ( 412.3 ) lbs. x 1000 | 182 (187) t |
| Max. zero fuel weight | 381.4 ( 392.4 ) lbs. x 1000 | 173 (178) t |
| Maximum fuel capacity | 36 750 US gal. | 139,100 l |
| Typical operating weight empty | 239.6 lbs. x 1000 | 108.7 t |
| Typical volumetric payload | 152.8 lbs. x 1000 | 69.3 t |
