Technical Data Airbus A340-300
Aircraft Dimensions
| ft | m | |
| Overall length | 208ft. 10in. | 63.6 |
| Height | 55ft. 3in. | 16.85 |
| Fuselage diameter | 18ft. 6in. | 5.64 |
| Maximum cabin width | 17ft. 4in. | 5.28 |
| Cabin length | 165ft. 3in. | 50.35 |
| 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 | 84ft. | 25.60 |
| Wheel track | 35ft. 1in. | 10.69 |
Basic Operation Data
| imperial | metric | |
| Engines | four CFM56-5C4/P | four CFM56-5C4/P |
| Engine thrust range | 31 200-34 000 lb. slst | 139-151 kN |
| Typical passenger seating | 295 | 295 |
| Range (max. pax) | 7 200 (7 400) nm | 13,350 (13,700) 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 | 608.3 (611.5) lbs. x 1000 | 275.9 (277.4) t |
| Max. take-off weight | 606.0 (609.6) lbs. x 1000 | 275 (276.5) t |
| Max. landing weight | 418.9 (423.3) lbs. x 1000 | 190 (192) t |
| Max. zero fuel weight | 392.4 (399) lbs. x 1000 | 178 (181) t |
| Maximum fuel capacity | 37 150 (39 060) US gal. | 140,640 (147,850) l |
| Typical operating weight empty | 285 (287) lbs. x 1000 | 129.3 (130.2) t |
| Typical volumetric payload | 95.9 (90.5) lbs. x 1000 | 43.5 (41) t |
