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Piper PA-12 Super Cruiser

From Wikipedia, the free encyclopedia
(Redirected fromPiper PA-12)
1940s American light aircraft
PA-12 Super Cruiser
PA-12 on skis
General information
TypePersonal use aircraft
National originUnited States
ManufacturerPiper Aircraft
StatusProduction completed
Primary userprivate owners
Number built3760[1]
History
Manufactured1946-1948
Introduction date1946
First flight29 October 1945
Developed fromPiper J-5
VariantsPiper PA-14
Backcountry Super Cubs Supercruiser

ThePiper PA-12 Super Cruiser is an American three-seat, high wing, single-engineconventional landing gear-equipped light aircraft that was produced byPiper Aircraft between 1946-48. The PA-12 was an upgraded and redesignatedPiper J-5.[2]

Development

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When Piper dropped the J- designation system in exchange for the PA- system, the J-5C became the PA-12 "Super Cruiser". The earlier J-5s had been powered by either a 100 hp (75 kW)Lycoming O-235 or a 75 hp (56 kW)Lycoming O-145. The newer PA-12 model was initially powered by a 108 hp (81 kW) Lycoming O-235-C engine, was fully cowled, and had a metal spar wing with two 19 gallon fuel tanks. A Lycoming O-235-C1 engine rated at 115 hp (86 kW) for takeoff was optional.[2][3]

The prototypeNX41561 was converted from a J-5C and first flew fromLock Haven, Pennsylvania, on 29 October 1945. The first production model followed on 22 February 1946 and quantity production continued until the last example of 3760 built was completed on 18 March 1948.[4]

The PA-12 is approved for wheels, skis, floats and also forcrop spraying.[3]

Cockpit accommodation is provided for the pilot in the front seat and two passengers in the rear seat, side-by-side. Unlike the J-3 Cub the PA-12 is flown solo from the front seat.[2][3]

Operational use

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PA-12 landing
PA-12 on floats

Many PA-12s have been modified with larger engines. Wing flaps and a metal-skin fuselage can be added as modifications.[3]

In 1947, two PA-12s, namedCity of Washington andCity of the Angels, flew around the world. The worst mechanical failure they suffered was a cracked tailwheel. TheCity of Washington currently resides at the Boeing Aviation Hangar, part of theSteven F. Udvar-Hazy Center inChantilly, Virginia. TheCity of the Angels is on display at thePiper Aviation Museum inLock Haven, Pennsylvania.[5]

PA-12s have been exported to a number of countries including Belgium, Canada, France, Ireland, Netherlands, Switzerland and the United Kingdom. Many PA-12s are still flown by private pilot owners and the type is commonly seen in North America. In November 2009 there were still 1688 registered in the US and 229 inCanada.[2][6][7]

Variants

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PA-12
Original modeltype certified 24 March 1947, with a gross weight of 1,750 lb (794 kg) in the Normal Category and 1,500 lb (680 kg) in the Utility Category[3]
PA-12S
Second model type certified 11 August 1948, with 1,838 lb (834 kg) gross weight, Normal Category only[3] The PA-12S Seaplane variant was fitted with the 135 hp (101 kW)Lycoming O-290-D2 engine to improve take-off performance.[8]

Notable accidents

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Specifications (PA-12)

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3-view line drawing of the Piper PA-12 Super Cruiser
3-view line drawing of the Piper PA-12 Super Cruiser

Data from Jane's All the World's Aircraft 1948[10]

General characteristics

  • Crew: one, pilot
  • Capacity: two passengers
  • Length: 22 ft 10 in (6.96 m)
  • Wingspan: 35 ft5+12 in (10.81 m)
  • Height: 6 ft 10 in (2.08 m)
  • Wing area: 179.3 sq ft (16.66 m2)
  • Empty weight: 950 lb (431 kg)
  • Gross weight: 1,750 lb (794 kg)
  • Max takeoff weight: 1,753 lb (795 kg)
  • Fuel capacity: 38 US gal (32 imp gal; 140 L)
  • Powerplant: 1 ×Lycoming O-235-C 4-cylinder air-cooled horizontally-opposed piston engine, 104 hp (78 kW)
  • Propellers: 2-bladed Sensenich fixed-pitch wooden propeller, 6 ft 2 in (1.88 m) diameter

Performance

  • Maximum speed: 91 kn (105 mph, 169 km/h) at sea level
  • Stall speed: 43 kn (49 mph, 79 km/h) (landing speed)
  • Range: 520 nmi (600 mi, 970 km)
  • Service ceiling: 18,000 ft (5,500 m) (absolute) at 1,550 lb (700 kg)
  • Rate of climb: 510 ft/min (2.6 m/s)
  • Wing loading: 9.76 lb/sq ft (47.7 kg/m2)
  • Take-off Run: 480 ft (150 m) at 1,550 lb (700 kg)
  • Landing Roll: 360 ft (110 m) at 1,550 lb (700 kg)

See also

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Related development

References

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  1. ^Peperell, 1987, P. 58
  2. ^abcdPlane and Pilot:1978 Aircraft Directory, page 59. Werner & Werner Corp, Santa Monica CA, 1977.ISBN 0-918312-00-0
  3. ^abcdefFederal Aviation Administration (March 2001)."AIRCRAFT SPECIFICATION NO. A-780 Revision 13"(PDF). Retrieved2011-02-22.
  4. ^Peperell, 1987, pp 58-59
  5. ^"Piper PA-12 Super Cruiser".Collections. Smithsonian National Air and Space Museum. Archived fromthe original on 24 June 2015. Retrieved9 June 2012.
  6. ^Federal Aviation Administration (November 2009)."FAA REGISTRY Make / Model Inquiry Results". Retrieved2009-11-03.
  7. ^Transport Canada (November 2009)."Civil Aircraft Register". Retrieved2009-11-03.
  8. ^Peperell, 1987, p. 58
  9. ^Hollander, Zaz; Brooks, James (1 August 2020)."State lawmaker and local pilot among 7 killed in midair collision over Alaska's Kenai Peninsula".Anchorage Daily News. Retrieved19 August 2020.
  10. ^Bridgman 1948, pp. 310c–311c

Bibliography

[edit]
  • Bridgman, Leonard (1948).Jane's All the World's Aircraft 1948. London: Sampson Low, Marston & Company, Ltd.
  • Peperell, Roger W. and Smith Colin R.,Piper Aircraft and their forerunners, 1987, Air-Britain (Historians) Ltd, Tonbridge, Kent,ISBN 0-85130-149-5.

External links

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