Technical Data Airbus A340-600
Aircraft Dimensions
| ft | m | |
| Overall length | 247ft. 1in. | 75.3 |
| Height | 56ft. 9in. | 17.3 |
| Fuselage diameter | 18ft. 6in. | 5.64 |
| Maximum cabin width | 17ft. 4in. | 5.28 |
| Cabin length | 200ft. 1in. | 60.98 |
| 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 | 107 ft. 11in. | 32.89 |
| Wheel track | 35ft. 1in. | 10.69 |
Basic Operation Data
| imperial | metric | |
| Engines | RR Trent 500 | RR Trent 500 |
| Engine thrust range | 56 000 (60 000) lb. slst | 249 (267) kN |
| Typical passenger seating | 380 | 380 |
| Range (max. pax) | 7 750 (7 900) nm | 14,360 (14,600) 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 | 813.9 (840.4) lbs. x 1000 | 369.2 (381.2) t |
| Max. take-off weight | 811.3 (837.8) lbs. x 1000 | 368 (380) t |
| Max. landing weight | 571 (584.2) lbs. x 1000 | 259 (265) t |
| Max. zero fuel weight | 540.1 (553.4) lbs. x 1000 | 245 (251) t |
| Maximum fuel capacity | 51 746 (54 023.2) US gal. | 195,881 (204,500) l |
| Typical operating weight empty | 392.0 (400.9) lbs. x 1000 | 177.8 (181.9) t |
| Typical volumetric payload | 122.6 lbs. x 1000 | 55.6 t |
