A300 B4-100

Aircraft type

Data given for the Airbus A300 B4-100 in basic configuration.

The Airbus A300 B4-100 is a variant of the Airbus A300 B2-100 with an additional fuel tank in the wing centre box, Krüger flaps at the wing root, and increased 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
58,100 l
15,350 us gal
Performance
Service ceiling
40,000 ft
12,190 m
Speed limits
Mmo
0.86
Vmo
360 kt
667 km/h / 414 mph
Weight limits
MLW
133,000 kg
293,210 lb
MTOW
150,000 kg
330,690 lb
MTW
150,900 kg
332,680 lb
MZFW
122,000 kg
268,960 lb

Engine models

Manufacturer Name Cont. T/O
General Electric CF6-50C 205.95 kN 224.19 kN
General Electric CF6-50C1 205.95 kN 230.42 kN
General Electric CF6-50C2 205.95 kN 230.42 kN
General Electric CF6-50C2D 205.95 kN 230.42 kN
General Electric CF6-50C2R - -
Pratt & Whitney JT9D-59A 199.15 kN 230.06 kN