Airbus A310

Airbus SAS

Airbus A310 aircraft
Airbus SASAirbus A310
Photo: Anidaat · CC BY-SA 4.0 · Modified

Details

The Airbus A310 is a shortened A300 with a new, smaller wing and the first two-crew flight deck on a widebody. Seven metres shorter than the A300 and carrying about seventy fewer passengers, it was built for thinner long routes, and it was among the first twins cleared for ETOPS across the Atlantic. Its cockpit is the one the A300-600 then adopted and the ancestor of the A330's. 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.

2

Variants

255

Built

Weightscompared to Airbus A380-800

MRW (Maximum Ramp Weight)

164,900kg
0
200k
400k
577k

MTOW (Maximum Takeoff Weight)

164,000kg
0
200k
400k
575k

MLW (Maximum Landing Weight)

124,000kg
0
150k
300k
395k

MZFW (Maximum Zero Fuel Weight)

116,500kg
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 CF6-80C2 or Pratt & Whitney JT9D-7R4 / PW4000

Fuel & Cargo

Fuel Capacity

61,090 L

Cargo Volume

112.2 m³

Production & History

Total Produced

255

Production Status

Out of production

First Flight

April 3, 1982