History
The A310 first began life as the A300B10, one of a number of projected developments and derivatives of Airbus' original A300B airliner.
While based on the larger A300, the A310 introduced a number of major changes. The fuselage was shortened by 13 frames compared to the A300B, reducing seating to around 200 to 230 passengers and a new higher aspect ratio wing of smaller span and area was developed. New and smaller horizontal tail surfaces, fly-by-wire outboard spoilers and a two crew EFIS flightdeck were incorporated, while the engine pylons were common to suit both engine options.
The first flight of the A310 occurred on April 3 1982, after the program was launched in July 1978. Service entry was with Lufthansa in April 1983. Early production A310s did not have the small winglets that became a feature of later build A310-200s and the A310-300. The A310-300 is a longer range development of the base A310-200, and has been in production since 1985. This version can carry a further 7000kg (15,430lb) of fuel in the tailplane.
The A310-200F freighter is available new build or as a conversion of existing aircraft (13 A310s were converted to freighters for Federal Express by Airbus partner Daimler Benz [now DaimlerChrysler] Aerospace Airbus). The A310-200C convertible passenger/freighter first entered service with Dutch operator Martinair in 1984.
Production
Total orders held for the A310 stood at 261 at late 1998, of which more than 250 had been delivered.
Capacity
Flightcrew of two. Max passenger capacity at nine abreast 280. Typical two class arrangement for 20 passengers at six abreast and 192 economy class passenger eight abreast. Cargo capacity in fore and aft underfloor compartments can hold 2.44 x 3.17m (88 x 125in) pallets or a total of up to 14 LD3 containers.
Dimensions
Wing span 43.89m (144ft 0in), length 46.66m (153ft 1in), height 15.80m (51ft 10in). Wing area 219.0m2 (2357.3sq ft).
Weights
A310-200 with CF6-80C2A2s - Operating empty 80,142kg (176,683lb), max takeoff 142,000kg (313,055lb). A310-300 with CF6-80C2A8s - Operating empty 81,205kg (179,025lb), max takeoff 150,000kg (330,695lb) standard, or higher gross weight options through to 164,000kg (361,560lb).
Performance
Max cruising speed 897km/h (484kt), long range cruising speed 850km/h (459kt). Range at typical airliner operating weight with 218 passengers and baggage and reserves 6800km (3670nm) for A310-200, 7982km (4310nm) for CF6 powered A310-300, 9580km (5170nm) for high gross weight A310-300 with CF6s.
Power Plants
Initial powerplant choice of either two 213.5kN (48,000lb) Pratt & Whitney JT9D-7R4D1s or two 222.4kN (50,000lb) General Electric CF6-80A3 turbofans. Current choices of 238kN (53,500lb) CF6-80C2A2s, 262.4kN (59,000lb) CF6-80C2A8s, 231.2kN (52,000lb) PW-4152s, or 249.1kN (56,000lb) PW-4156s.