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Ercoupe front I

The Ercoupe was the first aircraft certified by the Civil Aeronautics Administration (CAA) as "characteristically incapable of spinning." Lacking rudder pedals, the Ercoupe was flown using only the control wheel. A two-control system linked the rudder and aileron systems, which controlled yaw and roll, with the steerable nosewheel. The control wheel controlled the pitch and the steering of the aircraft, both on the ground and in the air, simplifying control and coordinated turning and eliminating the need for rudder pedals. The ERCO Ercoupe was first flown in 1937. It was designed to be the safest fixed-wing aircraft that aerospace engineering could provide at the time, and the type continues to enjoy a faithful following.

Ercoupe front II

General characteristics
Crew: one
Capacity: one passenger
Length: 20 ft 9 in (6.32 m)
Wingspan: 30 ft 0 in (9.14 m)
Height: 5 ft 11 in (1.80 m)
Powerplant: 1 × Continental C75-12 4-cylinder air-cooled horizontally-opposed piston engine, 75 hp (56 kW)

Ercoupe left I

Performance
Maximum speed: 110 mph (180 km/h, 96 kn)
Cruise speed: 95 mph (153 km/h, 83 kn)
Range: 300 mi (480 km, 260 nmi)

Ercoupe right rear I

Information sourced from Wikipedia

Edited by Feuer Zug
Text added

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