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Sud Aviation GY-80 Horizon

General Aviation and Light Aircraft

The GY-80 Horizon was a French four-seat touring monoplane of the 1960s, designed by Yves Gardan during the 1950s. In 1960 Sud Aviation acquired a licence to build the design from Gardan, and the prototype first flew on 21 July 1960. Sud Aviation built the aircraft at Nantes and Rochefort, and after it bought the bankrupt Morane-Saulnier company and formed the SOCATA subsidiary in 1966, production of its general aviation aircraft moved there. By the end of 1974, when production ended, Sud Aviation and SOCATA had built 273 of them. It was an all-metal low-wing design with Fowler-type flaps and partly retracting tricycle landing gear, powered by a Lycoming O-320 or O-360 flat-four piston engine. Most were bought by French private pilot owners, with exports to Germany, Switzerland and the United Kingdom, and an improved variant went on to become the SOCATA ST 10 Diplomate.

Facts
Year
1960 1
Engine Class
Piston 1
Status
Out of production 1
Power (kW)
130 1
Units Built
273 1
Top Speed (km/h)
250 1
Mass (kg)
625 1
Maximum Mass (kg)
1150 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Source SOCATA Horizon (Wikipedia)

Of Make

Source SOCATA Horizon (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source SOCATA Horizon (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
built under licence, first by Sud Aviation, and later by that company's SOCATA subsidiary

Originated In

Also in Geography Atlas: where this subject originated.

Source SOCATA Horizon (Wikipedia)Lead
Quote, Lead
The GY-80 Horizon is a French four-seat touring monoplane of the 1960s
Sources
1. SOCATA Horizon (Wikipedia)
  • Design and development, first flight
    The prototype first flew on 21 July 1960
  • Design and development, production
    manufactured 273 units by the end of 1974, when production was terminated
  • Lead
    The GY-80 Horizon is a French four-seat touring monoplane of the 1960s
  • Specifications, powerplant
    1 × Lycoming O-360-A flat-four piston engine, 130 kW (180 hp)
  • Specifications, power
    1 × Lycoming O-360-A flat-four piston engine, 130 kW (180 hp)
  • Specifications, empty weight
    Empty weight: 625 kg (1,378 lb)
  • Specifications, maximum take-off weight
    Max takeoff weight: 1,150 kg (2,535 lb)
  • Specifications, performance
    Maximum speed: 250 km/h (160 mph, 130 kn) at sea level
  • Lead, manufacturer
    built under licence, first by Sud Aviation, and later by that company's SOCATA subsidiary
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