A300 B1

Aircraft type

Data given for the Airbus A300 B1 in basic configuration.

The Airbus A300 B1 is the initial prototype of the Airbus A300 B2-100 with a shorter fuselage. Only two aircraft were built.

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
51 m
167.32 ft
Wing area
260 m²
2,798.64 sq ft
Wingspan
44.83 m
147.08 ft
Fuel
Fuel capacity
44,000 l
11,620 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
122,000 kg
268,960 lb
MTOW
137,000 kg
302,030 lb
MTW
137,900 kg
304,020 lb
MZFW
116,500 kg
256,840 lb

Aircraft models

Manufacturer Name
Airbus A300 B1
Prototype

Engine models

Manufacturer Name Cont. T/O
General Electric CF6-50A 205.95 kN 215.29 kN
General Electric CF6-50C 205.95 kN 224.19 kN