Airbus A320-211 Air Luxor CS-TNE
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Aircraft Data
The A320 is a twin engine short to medium range airliner. It was the first narrow body airliner produced by Airbus and first to use a fly-by-wire control system, with electronic cockpit and side-stick controller. Developed into a family of airliners.
The -200 was the definitive production version of the A320, with better range/payload performance compared to the series 100. Weights and engine thrusts were all increased.
| Country of Origin | First Flight | No. Built | No. In Service | Crew | Passengers |
|---|---|---|---|---|---|
| France | 1987 | 3000 | 3000 | 2 | 150 - 179 |
Power
Typical engine choices would be the CFM56-5B4 at 27000lb thrust or the V2500-A5 at 26500lb.
| Engine Count | 2 | ||
| Engine Variations | |||
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| Engine Name |
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Dimensions
| Length | 37.57 m. 123 ft. 3 in. |
| Wing Span | 34.09 m. 111 ft. 10 in. |
| Height | 11.84 m. 38 ft. 10 in. |
| Empty Weight | 42213 kg. 92980 lbs. |
| Max Weight | 77069 kg. 169755 lbs. |
Performance
| Max Speed | 784 kph 487 mph |
| Cruise Speed | 731 kph 454 mph |
| Ceiling | 12192 m. 40000 ft. |
| Normal Range | 4843 2615 nm km. |
| Max Range |
5639
3045
nm
km.
Performance figures for the A320-200 with CFM56 engines. |
Display data using: Metric Imperial
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