Aero / Ibis Aerospace Ae 270
Multi-Purpose Transport Aircraft
Photo ©: Karsten Palt
The Aero Ae 270 is a single-engine corporate and multi-purpose transport aircraft for up to 9 passengers developed by the Czech manufacturer AERO Vodochody Aerospace. It was planned to produce the Ae 270 in a joint venture called Ibis Aerospace together with AIDC from Taiwan. The project was cancelled in 2008 although full certification was received.
Propulsion | 1 Turboprop Engine |
Engine Model | Pratt & Whitney Canada PT6A-66A |
Engine Power | 634 kW | 850 shp |
Speed | 500 km/h | 270 kts 311 mph |
Service Ceiling | 9.144 m | 30.000 ft |
Range | 2.859 km | 1.544 NM 1.777 mi. |
Empty Weight | 2.564 kg | 5.653 lbs |
max. Takeoff Weight | 4.000 kg | 8.818 lbs |
Wing Span | 14,13 m | 46 ft 4 in |
Wing Area | 21,0 m² | 226 ft² |
Length | 12,32 m | 40 ft 5 in |
Height | 4,78 m | 15 ft 8 in |
First Flight | 25.07.2000 |
Production Status | no mass production |
ICAO Code | A270 |
EASA TCDS | A.060 |
Data for (Version) | IBIS/Aero Ae 270 |