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
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (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, manufacturerQuote, 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)LeadQuote, 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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