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Piper PA-6

The Piper PA-6 Sky Sedan was a 1940s American four-seat light aircraft designed and built in prototype form by Piper Aircraft at its Lock Haven, Pennsylvania, factory.[1]

PA-6 Sky Sedan
Role Light aircraft
Manufacturer Piper Aircraft
First flight 1944
Number built Two

History edit

Towards the end of 1944 Piper announced a number of aircraft types it intended to build after World War II. One of these was the PWA-6 Sky Sedan (Post War Airplane 6). A prototype was built in 1945 as a development of Piper's unsuccessful two-seat PT-1 trainer. Its fuselage had a fabric-covered metal frame with a four-seat cabin. It was a low-wing cantilever monoplane with a conventional tail unit and a retractable tailwheel landing gear. Originally to be powered by a 140 hp Franklin engine, it had a 165 hp Continental E-165 engine. By the time it first flew the designation had been changed to PA-6. A second aircraft was built in 1947, it differed by having an all-metal construction, a 205 hp Continental E-185 engine and a one-piece windscreen. Neither version was placed into production at a time when a short boom in postwar general aviation was ending.[2][3]

Specifications (PA-6) edit

Data from Jane's all the World's Aircraft 1947[4]

General characteristics

  • Crew: 1
  • Capacity: 3 pax
  • Length: 26 ft 0 in (7.93 m)
  • Wingspan: 34 ft 8 in (10.56 m)
  • Height: 7 ft 0 in (2.13 m)
  • Airfoil: Modified USA 35B
  • Empty weight: 1,360 lb (617 kg)
  • Gross weight: 2,400 lb (1,089 kg)
  • Fuel capacity: 40 US gal (33 imp gal; 150 L) fuel; 2.5 US gal (2.1 imp gal; 9.5 L) oil
  • Powerplant: 1 × Continental E165 6-cyl. horizontally-opposed air-cooled piston engine, 165 hp (123 kW)
  • Propellers: 2-bladed Sensenich fixed pitch propeller

Performance

  • Maximum speed: 160 mph (260 km/h, 140 kn)
  • Cruise speed: 150 mph (240 km/h, 130 kn) at 125 hp (93 kW) and 140 mph (120 kn; 230 km/h) at 100 hp (75 kW) at sea level
  • Economic cruising speed: 120 mph (100 kn; 190 km/h) at 40% power
  • Landing speed: 49 mph (43 kn; 79 km/h) with flaps; 55 mph (48 kn; 89 km/h) without flaps
  • Range: 620 mi (1,000 km, 540 nmi) at 140 mph (120 kn; 230 km/h)
  • Fuel consumption: 1.664 lb/mi (0.469 kg/km)

See also edit

Aircraft of comparable role, configuration, and era

References edit

Notes
  1. ^ Air Progress: 85. November 1978. {{cite journal}}: Missing or empty |title= (help)
  2. ^ Brady (2000), p.244
  3. ^ Bednarek, Dr. Janet. "General Aviation - An Overview", United States Centennial of Flight Commission 2012-09-15 at the Wayback Machine retrieved 11 August 2012
  4. ^ Bridgman, Leonard, ed. (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & Co. p. 278c.
Bibliography
  • Brady, Tim (2000). The American Aviation Experience: A History. Carbondale, Illinois: Southern Illinois University Press. ISBN 0-8093-2371-0.
  • 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, sedan, 1940s, american, four, seat, light, aircraft, designed, built, prototype, form, piper, aircraft, lock, haven, pennsylvania, factory, sedan, role, light, aircraft, manufacturer, piper, aircraft, first, flight, 1944, number, built, twohistory, edit. The Piper PA 6 Sky Sedan was a 1940s American four seat light aircraft designed and built in prototype form by Piper Aircraft at its Lock Haven Pennsylvania factory 1 PA 6 Sky Sedan Role Light aircraft Manufacturer Piper Aircraft First flight 1944 Number built TwoHistory editTowards the end of 1944 Piper announced a number of aircraft types it intended to build after World War II One of these was the PWA 6 Sky Sedan Post War Airplane 6 A prototype was built in 1945 as a development of Piper s unsuccessful two seat PT 1 trainer Its fuselage had a fabric covered metal frame with a four seat cabin It was a low wing cantilever monoplane with a conventional tail unit and a retractable tailwheel landing gear Originally to be powered by a 140 hp Franklin engine it had a 165 hp Continental E 165 engine By the time it first flew the designation had been changed to PA 6 A second aircraft was built in 1947 it differed by having an all metal construction a 205 hp Continental E 185 engine and a one piece windscreen Neither version was placed into production at a time when a short boom in postwar general aviation was ending 2 3 Specifications PA 6 editData from Jane s all the World s Aircraft 1947 4 General characteristicsCrew 1 Capacity 3 pax Length 26 ft 0 in 7 93 m Wingspan 34 ft 8 in 10 56 m Height 7 ft 0 in 2 13 m Airfoil Modified USA 35B Empty weight 1 360 lb 617 kg Gross weight 2 400 lb 1 089 kg Fuel capacity 40 US gal 33 imp gal 150 L fuel 2 5 US gal 2 1 imp gal 9 5 L oil Powerplant 1 Continental E165 6 cyl horizontally opposed air cooled piston engine 165 hp 123 kW Propellers 2 bladed Sensenich fixed pitch propeller Performance Maximum speed 160 mph 260 km h 140 kn Cruise speed 150 mph 240 km h 130 kn at 125 hp 93 kW and 140 mph 120 kn 230 km h at 100 hp 75 kW at sea level Economic cruising speed 120 mph 100 kn 190 km h at 40 power Landing speed 49 mph 43 kn 79 km h with flaps 55 mph 48 kn 89 km h without flaps Range 620 mi 1 000 km 540 nmi at 140 mph 120 kn 230 km h Fuel consumption 1 664 lb mi 0 469 kg km See also editAircraft of comparable role configuration and era Globe SwiftReferences edit nbsp Wikimedia Commons has media related to Piper aircraft Notes Air Progress 85 November 1978 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Brady 2000 p 244 Bednarek Dr Janet General Aviation An Overview United States Centennial of Flight Commission Archived 2012 09 15 at the Wayback Machine retrieved 11 August 2012 Bridgman Leonard ed 1947 Jane s all the World s Aircraft 1947 London Sampson Low Marston amp Co p 278c Bibliography Brady Tim 2000 The American Aviation Experience A History Carbondale Illinois Southern Illinois University Press ISBN 0 8093 2371 0 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 Retrieved from https en wikipedia org w index php title Piper PA 6 amp oldid 1094489811, wikipedia, wiki, book, books, library,

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