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Float-equipped PA-11S at Seattle Renton in 1973. A small number of PA-11s have been modified to use a Tricycle landing gear. [3]The PA-11 was one of the first aircraft to be used by Piper for experiments with the nose wheel (also known as tricycle gear) configuration.
The Piper PA-12 Super Cruiser is an American three-seat, high wing, single-engine conventional landing gear-equipped light aircraft that was produced by Piper Aircraft between 1946-48. The PA-12 was an upgraded and redesignated Piper J-5 .
The PA-44 is a development of the Piper Cherokee single-engined aircraft and is primarily used for multi-engined flight training. [ 2 ] [ 3 ] The Seminole has been built in three production runs; from 1979 to 1982, 1989 to 1990, and continuously since 1995.
Piper Airplane Parts Catalog: PA-31 Navajo, PA-31-300 Navajo, PA-31-325 Navajo C/R; September 10, 2009. Piper Aircraft Corporation, Manual Part Number 753-703; Piper Navajo Information Manual, Revision 9, March 18, 1994. Piper Aircraft Corporation, Manual Part Number 761-723; Piper Navajo Pilot's Operating Manual, Revision 34, April 22nd 2002.
The PA-16 Clipper is a stretched and refined version of the Vagabond intended to seat four people [1] (or "two-and-a-half to three" as often told by Clipper pilots). It is equipped with an extra wing tank, added doors to accommodate the new seating, and a Lycoming O-235, the same engine that would later power the Cessna 152.
The Piper PA-47 "PiperJet" was a single-engined very light jet (VLJ) that was intended to be developed and built by Piper Aircraft. However, following a change of ownership at Piper, it was decided to redesign the aircraft as the PiperJet Altaire. Despite being technically successful, the Altaire project was canceled in October 2011 due to ...
Data from Jane's All the World's Aircraft 1976–77 General characteristics Crew: 2 Capacity: 4–6 passengers Length: 34 ft 8 in (10.57 m) Wingspan: 42 ft 8 + 1 ⁄ 4 in (13.011 m) (over tip tanks) Height: 12 ft 9 in (3.89 m) Wing area: 229 sq ft (21.3 m 2) Airfoil: NACA 63 2 -415 at root, 63A212 at tip Empty weight: 4,870 lb (2,209 kg) Max takeoff weight: 9,000 lb (4,082 kg) Fuel capacity ...
In 1971, Piper built two Enforcers by heavily modifying two existing Mustang airframes, fitting them with Lycoming YT55-L-9A turboprop engines along with numerous other significant modifications. One airframe was a single seat (called the PE-1 and FAA registered as N201PE ), the other a dual-control aircraft (the PE-2 , registered N202PE ).