Aero Ae270
| Aero Ae270 | |
|---|---|
|
|
| Type: | Passenger plane |
| Design country: | |
| Manufacturer: | |
| First flight: |
July 25, 2000 |
The Aero Ae270 is a passenger or cargo aircraft with a pressurized cabin that was developed by the Czech company Aero . It arose from the original high-wing L-270 project. The first flight of the machine took place on July 25, 2000. The aircraft is being produced by a joint venture company from Aero with AIDC from Taiwan . AIDC (Aerospace Industrial Development Corporation) manufactures the wings and landing gear .
The Ae270P Ibis version is equipped with a Pratt & Whitney Canada engine. The avionics come from Allied-Signal Bendix / King.
In 2006 the certification according to FAR Part 23 and 36 took place.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1-2 |
| Passengers | 8-9 |
| length | 12.24 m |
| span | 13.80 m |
| height | 4.79 m |
| Wing area | 21 m² |
| Preparation mass | 1700 kg |
| Max. Takeoff mass | 3300 kg |
| Initial rate of climb | 8.2 m / s |
| Cruising speed | 333 km / h |
| Top speed | 381 km / h |
| Service ceiling | 9300 m |
| Range | 2200 km |
| Engines | 1 × Pratt & Whitney Canada PT6A with 850 PS (625 kW) (prototype with version PT6A-42A, series: PT6A-66A) and four-blade propeller |
| Unit price | approx. 2 million euros |
See also
literature
- Paul Jackson: Jane's All The World's Aircraft 2003-2004. Jane's Information Group, Coulsdon 2003, ISBN 0-7106-2537-5 .
Web links
Commons : Aero Ae270 - collection of images, videos and audio files
- EASA-TCDS-A.060 (PDF; 40 kB) - Type approval of Ae 270
- Page about the Aero A.38 (Czech)