Airbus A300B2
Airbus SAS

Photograph of the Airbus A300 family. No photograph on Wikimedia Commons identifies this variant specifically.
About
The first production A300, and the aeroplane that proved a twin-engined widebody could work. The heaviest certified B2 is the B2-320 of January 1980, on JT9D-59A engines, and that is the standard this row carries. It is a three-crew aeroplane: two pilots and a flight engineer, or two pilots on the aircraft modified to the forward-facing cockpit. Airbus publishes no airport-planning document for the B2, so its 44.84 m span and 53.49 m length come from the FAA's Aircraft Characteristics Database instead — and its height and empty weight are still not filled rather than guessed, because that database measures height at operating empty weight, which is a different thing. Cruise speed, range, ceiling and climb rate are EUROCONTROL's figures for the A30B 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 A300 B2-200 series from EASA TCDS A.172 (Airbus A300, A310, A300-600), issue 08, 1 February 2026, section 4.5: MMO 0.86.
Weightscompared to Airbus A380-800
Capacitycompared to Airbus A380-800
Passenger Capacity
40% of A380 maximum capacity
Crew
Dimensions
Length
Wingspan
Height
Engine Specifications
Engine Count
2×
Engine Model
Pratt & Whitney JT9D-59A
Fuel & Cargo
Fuel Capacity
44,400 L
Production & History
Production Status
Out of production
First Flight
June 28, 1973
Business jets and the API are coming
If you came here for the Airbus A300B2, you are the reader those are being built for. Leave an address and you will hear when they are ready.