Terzi T-9 Stiletto
| Terzi T-9 Stiletto | |
|---|---|
| Role | Two-seat light sport monoplane |
| National origin | Italy |
| Manufacturer | Terzi Aerodyne |
| Designer | Pietro Terzi |
| First flight | December 1990[1] |
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The Terzi T-9 Stiletto is an Italian two-seat light aircraft designed by Pietro Terzi and built by Terzi Aerodyne of Milan, Italy.[2]
Design and development
The Stiletto is a two-seat low-wing monoplane designed to meet the JAR-VLA regulations.[2] It is mainly metal construction but has a glassfibre cabin enclosure.[2] It has a fixed nosewheel landing gear and is powered by a nose mounted Rotax 912A piston engine.[2] The cantilever wings can be detached for transport and storage.[2]
Specifications
Data from [2]
General characteristics
- Crew: 1
- Capacity: 1
- Length: 6.85 m (22 ft 6 in)
- Wingspan: 10.26 m (33 ft 8 in)
- Height: 2.3 m (7 ft 7 in)
- Wing area: 12.3 m2 (132 sq ft)
- Aspect ratio: 8.558
- Empty weight: 380 kg (838 lb)
- Max takeoff weight: 650 kg (1,433 lb)
- Powerplant: 1 × Rotax 912A piston, 58 kW (78 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 200 km/h; 124 mph (108 kn)
- Cruise speed: 163 km/h; 101 mph (88 kn) 60% power
- Stall speed: 74 km/h; 46 mph (40 kn) with flaps
References
Notes
Bibliography
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