Technical Data Airbus A340-500
Aircraft Dimensions
| ft | m | |
| Overall length | 222ft. 8in. | 67.9 |
| Height | 56ft. 1in. | 17.1 |
| Fuselage diameter | 18ft. 6in. | 5.64 |
| Maximum cabin width | 17ft. 4in. | 5.28 |
| Cabin length | 175ft. 9in. | 53.56 |
| Wing span (geometric) | 208ft. 2in. | 63.45 |
| Wing area (reference) | 4,729 ft2 | 439.4 m2 |
| Wing sweep (25% chord) | 31.1 degrees | 31.1 degrees |
| Wheelbase | 90ft. 6in. | 27.59 |
| Wheel track | 35ft. 1in. | 10.69 |
Basic Operation Data
| imperial | metric | |
| Engines | four RR Trent 500 | four RR Trent 500 |
| Engine thrust range | 53 000 (56 000) lb. slst | 236 (249) kN |
| Typical passenger seating | 313 (3-class) | 313 (3-class) |
| Range (max. pax) | 8 670 (9 000) nm | 16,100 (16,700) 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 | 822.8 (840.4) lbs. x 1000 | 373.2 (381.2) t |
| Max. take-off weight | 820.1 (837.8) lbs. x 1000 | 372 (380) t |
| Max. landing weight | 535.7 (542.3) lbs. x 1000 | 243 (246) t |
| Max. zero fuel weight | 507.1 (511.5) lbs. x 1000 | 230 (232) t |
| Maximum fuel capacity | 56 750 (58 646) US gal. | 214,810 (222,000) l |
| Typical operating weight empty | 376.8 (385.4) lbs. x 1000 | 170.9 (174.8) t |
| Typical volumetric payload | 95.5 lbs. x 1000 | 43.3 t |
