Airbus A310-200
Airbus SAS

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. Maximum operating Mach number is the certificated figure for the A310-200 series from EASA TCDS A.172 (Airbus A300, A310, A300-600), issue 08, 1 February 2026, section 11.5: MMO 0.84.
Weightscompared to Airbus A380-800
Capacitycompared to Airbus A380-800
Passenger Capacity
32% of A380 maximum capacity
Crew
Dimensions
Length
Wingspan
Height
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
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