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 |