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Piper PT-1

General Aviation and Light Aircraft

The Piper PT-1 was a 1940s American two-seat primary training monoplane that Piper designed and built at Lock Haven. A low-wing tandem two-seater, it was the first Piper aircraft with a low wing. It had a fabric covering over an all-metal fuselage frame and wooden spar wings and tail, a retractable tailwheel landing gear, and a 130 horsepower Franklin 6AC engine. It had an empty weight of 1,325 pounds, a maximum speed of about 150 miles per hour and a range of 700 miles. No further aircraft were built, and a four-seat development, the Piper PWA-6 that became the PA-6 Sky Sedan, did not go into production either.

Facts
Engine Class
Piston 1
Status
One-off concept 1
Units Built
1 1
Top Speed (km/h)
240 1
Mass (kg)
601 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Source Piper PT-1 (Wikipedia)

Of Make

Source Piper PT-1 (Wikipedia)
Sources
1. Piper PT-1 (Wikipedia)
  • Lead, outcome
    No further aircraft were built.
  • Lead, number built
    No further aircraft were built.
  • Specifications (PT-1), powerplant
    Franklin 6AC-298 6-cyl. air-cooled horizontally-opposed piston engine, 130 hp (97 kW)
  • Lead
    is a 1940s American two-seat primary training monoplane
  • Specifications (PT-1), empty weight
    Empty weight: 1,325 lb (601 kg)
  • Specifications (PT-1), maximum speed
    Maximum speed: 150 mph (240 km/h, 130 kn)
  • Lead, manufacturer
    designed and built by Piper Aircraft at Lock Haven
  • Lead, country of origin
    is a 1940s American two-seat primary training monoplane designed and built by Piper Aircraft
  • Of Make: Piper Aircraft, Lead, make
    designed and built by Piper Aircraft at Lock Haven
  • In Group: Single-Engine Piston Light Aircraft, Lead, group placement
    is a 1940s American two-seat primary training monoplane
  • Exemplifies: General Aviation, Lead, mode placement
    primary training monoplane designed and built by Piper Aircraft
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