Airbus A300B4-103 Anatolia TC-GTA
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Aircraft Data
The A300 is a twin engined short/medium range wide-body airliner.It was the first airliner designed and built by Airbus,developed through a range of improved versions, Many have been converted to freighters. Production ceased in 2007.
The A300-B4 was the major early production version, with increased range compared to the B2, the B4 had its own developments - the -200 with further increased range and the -200FF, the first 2 crew edition of the A300.
| Country of Origin | First Flight | No. Built | No. In Service | Crew | Passengers |
|---|---|---|---|---|---|
| France | 1975 | 193 | 180 | 3 | 220 - 336 |
Power
Typical engines were the CF6-50C2 or the JT9D-9
| Engine Count | 2 | ||
| Engine Variations | |||
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Dimensions
| Length | 53.62 m. 175 ft. 11 in. |
| Wing Span | 44.83 m. 147 ft. 1 in. |
| Height | 16.48 m. 54 ft. 1 in. |
| Empty Weight | 88575 kg. 195100 lbs. |
| Max Weight |
165147 kg.
363760 lbs.
Weights for B4-200 version. |
Performance
| Max Speed | 797 kph 495 mph |
| Cruise Speed | 735 kph 457 mph |
| Ceiling | 10668 m. 35000 ft. |
| Normal Range | 5371 2900 nm km. |
| Max Range |
6297
3400
nm
km.
Range for B4-200 |
Display data using: Metric Imperial
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