Piper PT-1

PT-1 Trainer

Role	Monoplane trainer
Manufacturer	Piper Aircraft
First flight	1942
Number built	1

The Piper PT-1 was a 1940s American two-seat primary training monoplane designed and built by Piper Aircraft at Lock Haven. A low-wing tandem two-seat monoplane, the PT-1 was the first Piper aircraft to have a low-wing. It had a fabric covering over an all-metal fuselage frame and wooden spar wings and tail unit. The PT-1 had a retractable tailwheel landing gear and was powered by a 130 hp (97 kW) Franklin 6AC-2980D engine. No further aircraft were built. A four-seat development was designed as the Piper PWA-6 which did not go into production either.

Specifications (PT-1)

General characteristics

Crew: 2
Length: 22 ft 10 in ( m)
Wingspan: 35 ft 2½ in ( m)
Empty weight: 1325 lb ( kg)
Powerplant: 1 × Franklin 6AC-298-D, 130 hp ( kW)

Performance

Maximum speed: 150 mph ( km/h)
Range: 700 miles ( km)
Service ceiling: 12,400 ft ( m)

References

Wikimedia Commons has media related to Piper PT-1.

Roger W. Peperell and Colin M.Smith, Piper Aircraft and their forerunners, 1987, Air-Britain (Historians), ISBN 0-85130-149-5, Page 47 and 50.

Piper aircraft

Civilian	E-2 F-2 G-2 H-2 J-2 J-3 (Flitfire) J-4 J-5 M350 M500 M600 PA-6 PA-7 PA-8 PA-11 PA-12 PA-14 PA-15 PA-16 PA-17 PA-18 PA-19 PA-20 PA-22 PA-23 PA-24 PA-25 PA-26 PA-28 PA-29 PA-30 PA-31 PA-31T PA-32 PA-32R PA-33 PA-34 PA-35 PA-36 PA-38 PA-39 PA-40 PA-41 PA-42 PA-44 PA-46 PA-47 PA-60 PiperSport PT-1 PWA-1 PWA-6 PWA-8

Military	AE C-83 HE L-4 L-14 L-18 L-21 LNP NE O-59 PA-48 TG-8 U-7

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Piper PT-1

Specifications (PT-1)

See also

References