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Airbus A310
First flight year — 1982
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Airbus A310 Specifications
| 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 |
| Maximum cruise speed (km/h) | 850 | 850 |
| Maximum operating altitude (km) | 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 |
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