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The PA-28-161 Warrior II flying in the livery of the Singapore Youth Flying Club. At the time of the Cherokee's introduction, Piper's primary single-engined, all-metal aircraft was the Piper PA-24 Comanche, a larger, faster aircraft with retractable landing gear and a constant-speed propeller.
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Proposed single-engine turobprop variant of the Altaire PA-50 Freedom Family 0 Four-seat personal/trainer aircraft to replace the Cherokee PA-60 Aerostar: 1967 1,010 Six-seat pressurized twin, Piper purchased the design from Ted R. Smith: PiperSport: 2010 85 Two-seat light-sport aircraft marketed by Piper between January 2010 and January 2011.
A 1966 model Piper PA-32-260 Cherokee Six Piper PA-32-300. The Piper PA-32 Cherokee Six is a series of single-engine, fixed landing gear, light aircraft manufactured in the United States by Piper Aircraft between 1965 and 2007. [1] [2] The PA-32 is used around the world for private transportation, air taxi services, bush support, and medevac ...
Piper Aircraft Company factory in Lock Haven, Pennsylvania during the 1930s, with the Piper Cub logo superimposed at the top Piper PA-18-150 Super Cub.Built 1958. Piper PA-28-161 Warrior II Piper PA-34-200T Seneca Piper PA-31 Navajo airframe used for crash testing by NASA after a 1972 flood inundated Piper's factory Early-production PA-31 Navajo Piper PA-32RT-300T Turbo Lance II Piper PA-44 ...
The Piper PA-32R is a six-seat (or seven-seat), high-performance, single engine, all-metal, fixed-wing aircraft produced by Piper Aircraft of Vero Beach, Florida. The design began life as the Piper Lance, a retractable-gear version of the Piper Cherokee Six. Later models became known by the designation Piper Saratoga. The primary difference ...
The Piper PA-32RT-300T first left the assembly line in 1978-1979 and many are still being used today. This Piper is designated the Turbo Lance II. The single-engine plane can hold upwards of six ...
The LIO-320 is a "left-handed" version with the crankshaft rotating in the opposite direction for use on twin-engined aircraft to eliminate the critical engine. [2] [3] The first O-320 (with no suffix) was FAA certified on 28 July 1953 to CAR 13 effective 5 March 1952; this same engine was later re-designated, without change, as the O-320-A1A. [2]