SOCATA ST 10
| ST 10 Diplomate | |
|---|---|
 | |
| Role | Light aircraft |
| National origin | France |
| Manufacturer | SOCATA |
| First flight | 7 November 1967 |
| Produced | 1969-1974 |
| Number built | 55 |
| Developed from | Socata GY-80 Horizon |
The Socata ST-10 Diplomate was a French four-seat civil light aircraft. It was a development of the 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,[1] production beginning in 1970. Production ended in 1974, with a total of 55 built.[2]
Specifications (ST-10)
Data from [3]
General characteristics
- Crew: One pilot
- 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)
- Stall speed: 100 km/h[1] (55 knots, 63 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)
See also
Related development
Related lists
References
- Taylor, J.W.R. (ed.) Jane's All the World's Aircraft 1969-70. London:Sampson Low, 1969.
External links
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