Airbus A300B2

Airbus SAS

ICAOA30BIATAAB3
Airbus A300B2 aircraft
Airbus SASAirbus A300

Photograph of the Airbus A300 family. No photograph on Wikimedia Commons identifies this variant specifically.

Photo: 4300streetcar · CC BY 4.0 · Modified

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

MRW (Maximum Ramp Weight)

142,900kg
0
200k
400k
577k

MTOW (Maximum Takeoff Weight)

142,000kg
0
200k
400k
575k

MLW (Maximum Landing Weight)

136,000kg
0
150k
300k
395k

MZFW (Maximum Zero Fuel Weight)

126,000kg
0
150k
300k
369k

Capacitycompared to Airbus A380-800

Passenger Capacity

345passengers
0
300
600
853

40% of A380 maximum capacity

Crew

Total
3
Cockpit
3

Dimensions

Length

53.5m

Wingspan

44.8m

Height

16.5m

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

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