US two-seat high-wing light aircraft.

Function: sport plane, civil utility, trainer

Manufacturer: Piper Aircraft

Produced: 1938 –

Wingspan: 10,74 m

Lenght: 6,83 m

Max. takeoff weight: 550 kg

Max. speed: 140 km/h

Engine: Continental A-65-8 air-cooled horizontally opposed four cylinder, 48 kW

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