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The original Piper Aircraft company declared bankruptcy in 1991. In 1995, the New Piper Aircraft company was created. It was renamed Piper Aircraft once again in 2006. The company originally produced one variant, the 180-horsepower (134 kW) Archer LX (PA-28-181), [25] and began testing two diesel versions, with 135 and 155 hp. [26]
Piper PA-44-180 Seminole PA-44 landing Piper PA-44-180 Seminole. The Piper PA-44 Seminole is an American twin-engined light aircraft manufactured by Piper Aircraft. [2] The PA-44 is a development of the Piper Cherokee single-engined aircraft and is primarily used for multi-engined flight training. [2] [3]
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. It was produced by Czech Sport Aircraft and previously known as the ...
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 ...
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 PA-28 Cherokee light aircraft This page was last edited on 29 December 2019, at 16:43 (UTC). Text is available under the Creative Commons Attribution ...
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O-360-A1A 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1.The base model. A four-cylinder, horizontally opposed, air-cooled, direct-drive engine which includes provisions for supplying oil through the propeller shaft for installation of a single-acting controllable-pitch propeller.