Airbus A310-300 Iran Air
The A310 began its life as the A300B10, one of Airbus's A300B project designs. The A300-based aircraft is 13 frames shorter than the A300B, and this reduction in length has increased the number of passengers to 200 to 230. Also, the wing aspect ratio has increased and the aperture and wing area have decreased. The A310's cabin uses digital systems. With the help of these systems, the number of crew on the flight deck is reduced to 2 people, which is favorable for airlines. The first flight of the A310 took place on April 3, 1982, and in April 1983 entered service with Lufthansa Airlines. The A310-300 had a longer range based on the A310-200, and production began in 1985. Model 300 can carry up to 7000 kg of fuel. The A310-200F has also been introduced as a cargo model. Another model, the A310-200C, is a freight / passenger model first introduced in 1984 by the German company Martinhire. (This content is copied from the plane blog) Construction of such aircraft was halted in July 2007.
Credit to @GalacticaAsia for his original Airbus A310.300
The aircraft logo is made by @Augusta 81
Specifications
General Characteristics
- Predecessor A310-300[GE]
- Created On Android
- Wingspan 144.1ft (43.9m)
- Length 153.1ft (46.7m)
- Height 54.0ft (16.5m)
- Empty Weight N/A
- Loaded Weight 89,186lbs (40,454kg)
Performance
- Power/Weight Ratio 1.283
- Horse Power/Weight Ratio 0.033
- Wing Loading 26.9lbs/ft2 (131.5kg/m2)
- Wing Area 3,311.1ft2 (307.6m2)
- Drag Points 18563
Parts
- Number of Parts 2230
- Control Surfaces 9
- Performance Cost 7,495
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