A310-300

Aircraft type

Data given for the Airbus A310-300 in basic configuration.

The Airbus A310-300 is a variant of the Airbus A310-200 with an additional fuel tank in the horizontal stabilizer.

Manufacturer Airbus
Aircraft family Airplane
Engine type Turbofan
Engine count 2
ICAO code A310
IATA code 313

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
61,090 l
16,140 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
123,000 kg
271,170 lb
MTOW
150,000 kg
330,690 lb
MTW
150,900 kg
332,680 lb
MZFW
113,000 kg
249,120 lb

Engine models

Manufacturer Name Cont. T/O
General Electric CF6-80C2A2 213.87 kN 233.35 kN
General Electric CF6-80C2A8 213.87 kN 257.37 kN
Pratt & Whitney JT9D-7R4E1 211.29 kN 222.41 kN
Pratt & Whitney PW4152 218.85 kN 231.31 kN
Pratt & Whitney PW4156A 218.85 kN 249.10 kN