Samiksha Jaiswal (Editor)

SOCATA ST 10

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Top speed
  
280 km/h

Length
  
7.1 m

Manufacturer
  
DAHER-SOCATA

Wingspan
  
9.7 m

First flight
  
November 7, 1967

SOCATA ST 10 SOCATA ST 10 Wikipedia

Socata st 10 fly by in sweden


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, production beginning in 1970. Production ended in 1974, with a total of 55 built.

Contents

SOCATA ST 10 FileSocata ST10 Diplomate AN1064808jpg Wikimedia Commons

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Specifications (ST-10)

Data from

General characteristics

SOCATA ST 10 SOCATA ST10 Diplomate Specifications Technical Data Description

  • 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

    SOCATA ST 10 Socata ST10 Diplomate Specifications A photo

  • Maximum speed: 280 km/h (151 knots, 174 mph)
  • Cruise speed: 265 km/h (143 knots, 165 mph)
  • Stall speed: 100 km/h (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)

    • SOCATA ST 10 ST10 Diplomate Specifications A photo

    SOCATA ST 10 httpsiytimgcomvid0JnB8NBFkhqdefaultjpg

    SOCATA ST 10 FileSocata ST10 Diplomatejpg Wikimedia Commons

    References

    SOCATA ST 10 Wikipedia
    (Text) CC BY-SA


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