Aero Ae 270 Ibis
From Wikipedia, the free encyclopedia
The Aero Ae 270 Ibis is a turboprop-powered civil utility aircraft currently under development. Design work by Aero commenced in the early 1990s, with the aircraft's configuration finalised by 1993. In 1997, Aero signed an agreement with AIDC of Taiwan to jointly manufacture and market the aircraft as Ibis Aerospace.
Airworthiness has been certified by the Czech Civil Aviation Authority permitting training and aerial work, including commencement of commercial use[1].
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[edit] Specifications (Ae 270)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.Data from Ae270 Propjet Specifications
General characteristics
- Crew: One or two
- Capacity: Up to 10 passengers, but typically 6.
- Length: 12.23 m (40 ft 1 in)
- Wingspan: 13.82 m (45 ft 4 in)
- Height: 4.78 m (15 ft 8 in)
- Wing area: 21 m² (226 ft²)
- Airfoil: NASA MS(1)-0316.7 (root), NASA MS(1)-0312 (tip)[2]
- Empty weight: 2,564 kg (5,653 lb)
- Useful load: 1,136 kg (2,504 lb)
- Max takeoff weight: 4,000 kg (8,818 lb)
- Powerplant: 1× Pratt & Whitney Canada PT6A-66A-42A turboprop engine, 634 kW (850 shp)
- * Maximum landing weight: 3,800 kg (8,377 lb)
Performance
- Maximum speed: 500 km/h (270 knots, 311 mph) at 7,600 m (25,000 ft)
- Stall speed: 162 km/h (87.7 KEAS, 100 mph) with flaps up
- Range: 2,859 km (1,544 nm, 1,777 mi) at 30,000 ft with 30-minute VFR reserve
- Service ceiling 9,144 m (30,000 ft)
- Rate of climb: 8.0 m/s (1.581 ft/m)
- Wing loading: 190 kg/m² (38.9 lb/ft²)
[edit] References
- ^ "Ae270 Commercial Flight-Ready", Aviation Week & Space Technology, January 8, 2007.
- ^ The Incomplete Guide to Airfoil Usage
[edit] External links
- www.ae270.com – Official website
- Specs & Photo at Flugzeuginfo.net
[edit] See also
Comparable aircraft
- Myasichtchev 101
- Pilatus PC-12
- Piper Meridian
- Socata TBM 700
Related lists
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