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A 3-view drawing of a Piper PA-28R-200 Cherokee Arrow PA-28R-180 Cherokee Arrow Four-place, retractable landing gear landplane, Lycoming IO-360-B1E engine of 180 hp (134 kW), gross weight 2,500 lb (1,134 kg). First certified on 8 June 1967. [19] Built in the following variants: PA-28R-180 Cherokee Arrow, initial version. [35]
PA-26 0 Proposed higher-power version of the PA-24 PA-27 Aztec: 1960 4,930 Improved version of the PA-23, kept PA-23 designation PA-28 Cherokee: 1961 10,896 Single-engined low-wing cabin monoplane PA-28-140 Cherokee: 1964 10,089 Two-seat training variant PA-28 Warrior: 1974 4,842 Improved PA-28 PA-28-235 Cherokee/Dakota: 1964 2,913 Higher-power ...
Piper PA-28 Cherokee light aircraft Topics referred to by the same term This disambiguation page lists articles associated with the same title formed as a letter–number combination.
Print/export Download as PDF; Printable version; In other projects Wikimedia Commons; ... Piper PA-28 Cherokee; Piper PA-31T Cheyenne; Piper PA-42 Cheyenne; Taylor ...
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 Seneca-200T 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-32-RT-300T Turbo Lance II Piper PA-44 ...
The PA-28R-300 Pillán was developed by Piper Aircraft in the United States as a two-seat military trainer for assembly in Chile, based on a PA-32R fuselage with a new center-section and wing stressed for aerobatics. [4] The first prototype designated XBT first flew at Lakeland on 6 March 1981 and was followed by a second prototype, designated ...
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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 ...