A310-200C

Aircraft type

Data given for the Airbus A310-200C in basic configuration.

The Airbus A310-200C is a modification of the Airbus A310-200 with the addition of an upper deck cargo door.

Manufacturer Airbus
Aircraft family Airplane
Engine type Turbofan
Engine count 2
ICAO code A310

Technical specifications

Dimensions
Fuselage height
5.64 m
18.5 ft
Fuselage width
5.64 m
18.5 ft
Height
15.95 m
52.33 ft
Length
46.66 m
153.08 ft
Wing area
219 m²
2,357.32 sq ft
Wingspan
43.9 m
144.03 ft
Fuel
Fuel capacity
55,100 l
14,560 us gal
Performance
Service ceiling
41,100 ft
12,530 m
Speed limits
Mmo
0.84
Vmo
360 kt
667 km/h / 414 mph
Weight limits
MLW
121,500 kg
267,860 lb
MTOW
138,600 kg
305,560 lb
MTW
139,500 kg
307,540 lb
MZFW
111,500 kg
245,820 lb

Aircraft models

Manufacturer Name
Airbus A310-203C

Engine models

Manufacturer Name Cont. T/O
General Electric CF6-80A3 203.73 kN 217.83 kN