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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.
Download as PDF; Printable version; In other projects Wikidata item; ... PA-28 may refer to: Pennsylvania's 28th congressional district ; Pennsylvania Route 28, a ...
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 ...
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.
The CSA SportCruiser is a two-seat, single engine, tricycle undercarriage, fixed-wing aircraft that was introduced in 2006 by Czech Aircraft Works (CZAW), now named Czech Sport Aircraft. [3] [4] [5] In January 2010, the SportCruiser was added to the Piper Aircraft line as the PiperSport under a licensing agreement with Czech Sport Aircraft ...
A V16 engine is a sixteen-cylinder piston engine where two banks of eight cylinders are arranged in a V configuration around a common crankshaft. V16 engines are less common than engines with fewer cylinders, such as V8 and V12 engines. Each bank of a V16 engine can be thought of as a straight-eight, a design that can be inherently balanced ...
Data from Jane's all the World's Aircraft 1988–89 General characteristics Crew: 2 Length: 8 m (26 ft 3 in) Wingspan: 8.84 m (29 ft 0 in) Height: 2.64 m (8 ft 8 in) Wing area: 13.69 m 2 (147.4 sq ft) Airfoil: root: NACA 65 2 -415 ; tip: NACA 65 2 -415 modified Empty weight: 930 kg (2,050 lb) equipped Max takeoff weight: 1,338 kg (2,950 lb) (and Maximum Landing Weight) 1,315 kg (2,899 lb ...
The enclosed cabin has two tandem seats. Early PA-11s had a Continental A65-8 engine, while the later ones had the option of a Continental C90-8. [2] The PA-11 was based on the earlier J-3, but with the engine cowling fully enclosed (as on the earlier J-5), the windshield sloped at a shallower angle, and the fuel tank placed in the port wing ...