A300 B2-320

Aircraft type

Data given for the Airbus A300 B2-320 in basic configuration.

The Airbus A300 B2-320 is a variant of the Airbus A300 B2-200 with increased landing and zero fuel weights.

Manufacturer Airbus
Aircraft family Airplane
Engine type Turbofan
Engine count 2
ICAO code A30B

Technical specifications

Dimensions
Fuselage height
5.64 m
18.5 ft
Fuselage width
5.64 m
18.5 ft
Height
16.72 m
54.86 ft
Length
53.61 m
175.89 ft
Wing area
260 m²
2,798.64 sq ft
Wingspan
44.83 m
147.08 ft
Fuel
Fuel capacity
44,400 l
11,730 us gal
Performance
Service ceiling
40,000 ft
12,190 m
Speed limits
Mmo
0.86
Vmo
345 kt
639 km/h / 397 mph
Weight limits
MLW
136,000 kg
299,830 lb
MTOW
142,000 kg
313,060 lb
MTW
142,900 kg
315,040 lb
MZFW
126,000 kg
277,780 lb

Aircraft models

Manufacturer Name
Airbus A300 B2-320

Engine models

Manufacturer Name Cont. T/O
Pratt & Whitney JT9D-59A 199.15 kN 230.06 kN