Technical Data Airbus A330-200
Aircraft Dimensions
| ft | m | |
| Overall length | 188ft. 8in. | 58.8 |
| Height | 57ft. 1in. | 17.40 |
| Fuselage diameter | 18ft. 6in. | 5.64 |
| Maximum cabin width | 17ft. 4in. | 5.28 |
| Cabin length | 147ft. 8in. | 45.0 |
| Wing span (geometric) | 197ft. 10in. | 60.3 |
| Wing area (reference) | 3,892 ft2 | 361.6 m2 |
| Wing sweep (25% chord) | 30 degrees | 30 degrees |
| Wheelbase | 72ft. 10in. | 22.2 |
| Wheel track | 35ft. 11in. | 10.69 |
Basic Operation Data
| imperial | metric | |
| Engines | two CF6-80E1 or PW4000 or RR Trent 700 | two CF6-80E1 or PW4000 or RR Trent 700 |
| Engine thrust range | 68 000-72 000 lb. slst | 303-320 kN |
| Typical passenger seating |
253 (3-class) 293 (2-class) |
253 (3-class) 293 (2-class) |
| Range (max. pax) | 6 750 nm | 12,500 km |
| Max. operating Mach number (Mmo) | 0.86 Mo. | 0.86 Mo. |
| Bulk hold volume - Standard/option | 695 / 486 ft3 | 19.7 / 13.76 m3 |
Design Weights
| imperial | metric | |
| Max. ramp weight | 509 (515.7) lbs. x 1000 | 230.9 (233.9) t |
| Max. take-off weight | 507 (513.7) lbs. x 1000 | 230 (233) t |
| Max. landing weight | 396.8 (401.2) lbs. x 1000 | 180 (182) t |
| Max. zero fuel weight | 370.4 (374.8) lbs. x 1000 | 168 (170) t |
| Maximum fuel capacity | 36 750 US gal. | 139,100 l |
| Typical operating weight empty | 263.7 lbs. x 1000 | 119.6 t |
| Typical volumetric payload | 80.2 lbs. x 1000 | 36.4 t |
