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The PA-32 series was developed to meet a requirement for a larger aircraft than the four-seat Piper PA-28 Cherokee. [3] The first prototype PA-32 made its initial flight on December 6, 1963, with the type being publicly announced in October 1964, with Federal Aviation Administration (FAA) aircraft type certification following on March 4, 1965. [4]
Two-seat low wing twin-boom monoplane, later became PA-7 PWA-8 Cub Cycle: 1944 1 Single-seat, mid-wing single-engine monoplane LBP: 1945 3 Single-seat, optionally-piloted glider bomb PA-6 Sky Sedan: 1945 2 Four-seat, low-wing retractable gear monoplane PA-7 Skycoupe: 1944 1 Two-seat low wing twin-boom monoplane, was PWA-1, PA-8 Skycycle: 1945 2
An aircraft seat map or seating chart is a diagram of the seat layout inside a passenger airliner.They are often published by airlines for informational purposes and are of use to passengers for selection of their seat at booking or check-in.
Towards the end of 1944 Piper announced a number of aircraft types it intended to build after World War II. One of these was the PWA-6 Sky Sedan (Post War Airplane 6). A prototype was built in 1945 as a development of Piper's unsuccessful two-seat PT-1 trainer. Its fuselage had a fabric-covered metal frame with a four-seat cabin.
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-34 Seneca is a twin-engined light aircraft, produced in the United States by Piper Aircraft.It has been in non-continuous production since 1971. [4] [5] [6] The Seneca is primarily used for personal and business flying [1] as well as multi-engine class rating flight training.
The Piper PA-23, named Apache and later Aztec, is an American four- to six-seat twin-engined light aircraft aimed at the general aviation market. The United States Navy and military forces in other countries also used it in small numbers.
The 230 hp (172 kW) engine gives the aircraft a sea level, standard day takeoff distance of 150 ft (46 m) and a landing distance of 300 ft (91 m). [ 1 ] [ 2 ] The V6 STOL has a typical empty weight of 1,200 lb (540 kg) and a gross weight of 2,200 lb (1,000 kg), giving a useful load of 1,000 lb (450 kg).