AT-3
.jpg?width=800)
The Aero AT-3 is a two-seat, low wing, utility aircraft manufactured in Poland by Aero AT in ready-to-fly certificated form and as a kitplane. The aircraft is of conventional configuration and features fixed tricycle undercarriage. The structure is largely of all-metal construction. Designed by Tomasz Antoniewski it first flew in 1997 and deliveries to customers commenced in 2002. It is certified under the European Very Light Aircraft regulations. On July 2, 2010 Aero AT-3 was granted an American Federal Aviation Administration type certificate, based on its European VLA certification.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Aero AT
- Category
- Single-engine piston
- Country of origin
- Poland
- First flight
- 1997-01-01
Specifications
- Cruise speed
- 110 kt
- Max speed
- 120 kt
- Range
- 488 nm
- Service ceiling
- 12,500 ft
- Rate of climb
- 730 ft/min
- Max takeoff weight
- 1,283 lb
- Empty weight
- 772 lb
- Fuel capacity
- 18 US gal
- Powerplant
- Rotax 912S
- Engines
- 1
- Seats
- 2
- Length
- 19.3 ft
- Wingspan
- 24.8 ft
- Height
- 7.3 ft
- Number built
- 70
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.