Technical Data Airbus A310
Aircraft Dimensions
| ft | m | |
| Overall length | 153ft. 1in. | 46.66 |
| Height | 51ft. 10in. | 15.80 |
| Fuselage diameter | 18ft. 6in. | 5.64 |
| Maximum cabin width | 17ft. 4in. | 5.28 |
| Cabin length | 109ft. 1in. | 33.25 |
| Wing span (geometric) | 144ft. | 43.90 |
| Wing area (reference) | 2,360 ft2 | 219 m2 |
| Wing sweep (25% chord) | 28 degrees | 28 degrees |
| Wheelbase | 49ft.11in. | 15.21 |
| Wheel track | 31ft. 6in. | 9.60 |
Basic Operation Data
| imperial | metric | |
| Engines | two CF6-80C2 or PW4000 | two CF6-80C2 or PW4000 |
| Engine thrust range | 52 000-59 000 lb. slst | 230-260 kN |
| Typical passenger seating | 220 (2-class) | 220 (2-class) |
| Range (max. pax) | 4 350 (5 200) nm | 8,050 (9,600) km |
| Max. operating Mach number (Mmo) | 0.84 Mo. | 0.84 Mo. |
| Bulk hold volume - Standard/option | 610 (318) ft3 | 17.3 (9.0) m3 |
Design Weights
| imperial | metric | |
| Max. ramp weight | 332.7 (363.5) lbs. x 1000 | 150.9 (164.9) t |
| Max. take-off weight | 330.7 (361.6) lbs. x 1000 | 150 (164) t |
| Max. landing weight | 271.2 (273.4) lbs. x 1000 | 123 (124) t |
| Max. zero fuel weight | 249.1 (251.3) lbs. x 1000 | 113 (114) t |
| Maximum fuel capacity | 16 130 (19 940) US gal. | 61,070 (75,470) l |
| Typical operating weight empty | 178.8 (183.3) lbs. x 1000 | 81.1 (83.1) t |
| Typical volumetric payload | 58.9 (47.6) lbs. x 1000 | 26.7 (21.6) t |
