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Aircraft type: Commercial airplane
Manufacturer: Airbus
Maiden flight year: 1982
A310-200 | A310-300 | |
Dimensions | ||
---|---|---|
Length (m) | 46.7 | 46.7 |
Wingspan (m) | 43.9 | 43.9 |
Height (m) | 15.8 | 15.8 |
Wing area (m2) | 219 | 219 |
Weight | ||
Maximum take-off weight (kg) | 142 000 | 164 000 |
Maximum landing weight (kg) | 123 000 | 124 000 |
Operating empty weight (kg) | 79 450 | 82 600 |
Maximum zero fuel weight (kg) | 113 000 | 114 000 |
Maximum payload (kg) | 33 550 | 33 460 |
Standard fuel capacity (litres) | 54 920 | 75 470 |
Performance | ||
Maximum range (km) | 4 600 | 9 600 |
Range with max payload (km) | 4 000 | 5 600 |
Cruise speed (km/h) | 850 | 850 |
Maximum speed (km/h) | 900 | 900 |
Maximum operating altitude (m) | 12 200 | 12 200 |
Take-off field length (m) | 1 860 | 2 290 |
Landing field length (m) | 1 480 | 1 490 |
Engines | GE CF6-80C2A2, 2 x 53200 lbP&W JT9D-7R4, 2 x 50000 lb | GE CF6-80C2A8, 2 x 59000 lbP&W PW4156A, 2 x 56000 lb |
Fuel efficiency (g/pass*km) | 20.7 | 20.3 |
Fuel flow rate (kg/h) | 4 400 | 4 300 |
Cabin Data | ||
Passengers (1-class) | 279 | 279 |
Passengers (2-class) | 218 | 218 |
Passengers (3-class) | 187 | 187 |
Cabin width (m) | 5.28 | 5.28 |
27% | 33% | 40% |