Airbus A310
The Airbus A310 is a wide-body twin-engine aircraft that first took to the air on 3 April 1982. The Airbus A310 was a competitor in the market primarily to the Boeing 767-200.
technical parameters Airbus A310
| Manufacturer | Airbus |
| Role | Wide-body aircraft |
| First flight | 3 April 1982 |
| Introduction | April 1983 with Swissair |
| Primary users |
|
| Number built | 255 |
| Produced | 1981–1998 |
| Cockpit Crew | Two |
| 2-class | 220 passengers (20F + 200Y) |
| 1-class |
|
| Exit limit | 275 passengers |
| Lower deck | 14 LD3 containers |
| Wing | 43.9 m (144 ft) span, 219 m2 (2,360 sq ft) area, 28 ° sweep 8.8 aspect ratio |
| Length | 46.66 m (153 ft 1 in) |
| Height | 15.8 m (51 ft 10 in) fuselage |
| Cross section | 5.64 m (18 ft 6 in) |
|
Maximum takeoff weight |
|
| Empty weight | JT9D: 77.4 t (171,000 lb), PW4000/CF6-80: 79.2 t (175,000 lb) |
| Maximum Payload |
|
| Max fuel | 47,940 kg / 105 689 lb |
| Engines |
|
| Thrust (×2) | 203.8–257.4 kN (45,800–57,900 lbf) |
| Speed | Mach 0.8 (459 kn; 850 km/h) cruise, Mach 0.84 (482 kn; 892 km/h) MMO |
| Range |
|
| Ceiling | 41,100 ft (12,527 m) |
Airbus A310
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