Airbus A310-200

Airbus SAS

Airbus A310-200 aircraft
Airbus SASAirbus A310-200
Photo: Ilya Plekhanov · CC BY-SA 3.0 · Modified

About

The first A310, certified in March 1983 and in service the same year. It carries 55,100 litres in three tanks — the -300's tail trim tank came later — and seats 237 in a single class against a certified maximum of 275. Its two-crew flight deck was the first on a widebody and is what the A300-600 was rebuilt to use. Cruise speed, range, ceiling and climb rate are EUROCONTROL's figures for the A310 type code rather than a certificate's: a type certificate states limits and weights, not cruise performance, and the source does not distinguish sub-variants.

Weightscompared to Airbus A380-800

MRW (Maximum Ramp Weight)

144,900kg
0
200k
400k
577k

MTOW (Maximum Takeoff Weight)

144,000kg
0
200k
400k
575k

MLW (Maximum Landing Weight)

121,500kg
0
150k
300k
395k

MZFW (Maximum Zero Fuel Weight)

111,500kg
0
150k
300k
369k

Empty Weight

79,207kg
0
100k
200k
280k

Capacitycompared to Airbus A380-800

Passenger Capacity

275passengers
0
300
600
853

32% of A380 maximum capacity

Crew

Total
8
Cockpit
2
Cabin
6

Dimensions

Length

46.7m

Wingspan

43.9m

Height

15.9m

Engine Specifications

Engine Count

2×

Engine Model

General Electric CF6-80A3 / CF6-80C2 or Pratt & Whitney JT9D-7R4

Fuel & Cargo

Fuel Capacity

55,100 L

Cargo Volume

112.2 m³

Production & History

Production Status

Out of production

First Flight

April 3, 1982