A300 B2-200

Aircraft type

Data given for the Airbus A300 B2-200 in basic configuration.

The Airbus A300 B2-200 is a variant of the Airbus A300 B2-100 with the addition of Krüger flaps at the wing root.

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
44,000 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
130,000 kg
286,600 lb
MTOW
142,000 kg
313,060 lb
MTW
142,900 kg
315,040 lb
MZFW
120,500 kg
265,660 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 - -