Technical Data Airbus A340-200
Aircraft Dimensions
| ft | m | |
| Overall length | 194ft. 10in. | 59.39 |
| Height | 54ft. 9in. | 16.7 |
| Fuselage diameter | 18ft. 6in. | 5.64 |
| Maximum cabin width | 17ft. 4in. | 5.28 |
| Cabin length | 151ft. 1in. | 46.06 |
| Wing span (geometric) | 197ft. 1in. | 60.3 |
| Wing area (reference) | 3,892 ft2 | 361.6 m2 |
| Wing sweep (25% chord) | 30 degrees | 30 degrees |
| Wheelbase | 76ft. 3in. | 23.24 |
| Wheel track | 35ft. 1in. | 10.69 |
Basic Operation Data
| imperial | metric | |
| Engines | four CFM56-5C4 | four CFM56-5C4 |
| Engine thrust range | 31 200-34 000 lb. slst | 139-151 kN |
| Typical passenger seating | 239 | 239 |
| Range (max. pax) | 8 000 nm | 14,800 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 | 608.2 lbs. x 1000 | 275.9 t |
| Max. take-off weight | 606.3 lbs. x 1000 | 275 t |
| Max. landing weight | 407.9 lbs. x 1000 | 185 t |
| Max. zero fuel weight | 381.4 lbs. x 1000 | 173 t |
| Maximum fuel capacity | 40 960 US gal. | 155,040 l |
| Typical operating weight empty | 284.4 lbs. x 1000 | 129 t |
| Typical volumetric payload | 67.9 lbs. x 1000 | 30.8 t |
