Socata ST 10
From Wikipedia, the free encyclopedia
The Socata ST-10 Diplomate was a French four-seat civil light aircraft. It was a development of Socata's GY-80 Horizon, and was initially known as the Super Horizon 200, later the Provence, before finally being named the ST-10 Diplomate. The first prototype flew on 7 November 1967, production beginning in 1970.
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[edit] Specifications (ST-10)
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 [1]
General characteristics
- Crew: One pillot
- Capacity: Three passengers
- Length: 7.10 m (23 ft 3½ in)
- Wingspan: 9.69 m (31 ft 9¾ in)
- Height: 2.90 m (9 ft 5⅓ in)
- Wing area: 13.00 m² (139.93 ft²)
- Empty weight: 724 kg (1,594 lb)
- Max takeoff weight: 1,222 kg (2,689 lb)
- Powerplant: 1× Lycoming IO-360-C 4-cylinder horizontally-opposed fuel-injected piston engine, 149 kW (200 hp)
Performance
- Maximum speed: 280 km/h (151 knots, 174 mph)
- Cruise speed: 265 km/h (143 knots, 165 mph)
- Range: 1,200 km (648 nm, 746 mi) with four persons
- Service ceiling 5,000 m (16,400 ft)
- Rate of climb: 4.8 m/s (945 ft/min)
[edit] References
- ^ Green, William, The Observers Book of Aircraft, Frederick Warne & Co. Ltd, 1970. ISBN 0-7232-0087-4
[edit] External links
[edit] See also
Related development
- Socata GY-80 Horizon
Related lists
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