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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-28R-180B Cherokee Arrow B, as PA-28R-180 with minor changes ...
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 ...
In addition to aircraft parts, the company supplies parts and kits to construct several light aircraft designs, all based on 1930s and 1940s Piper Aircraft models. [1] [3] [4] [5] [8] The Wag-Aero CUBy, a Piper J-3 replica, was designed by Dick Wagner and first flew on 12 March 1975. It is offered in several different models and variants ...
180 hp (134 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 6.0:1. Uses a TCM 639230A3 or 6006 fuel injector. Same as IO-360-A except for reduced compression ratio and rated power. The crankshaft has two 6th order dampers. [4] IO-360-C 210 hp (157 kW) at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1.
The representative model should be a common one, and as I write this, there are more PA-28-140s on the FAA registry (4,321) than any other single PA-28 variant. I see no compelling reason to redo the specs. Carguychris 17:15, 10 April 2020 (UTC)
8 Piper PA-28-161 Cadet. 1 comment. 9 Image added. 2 comments. 10 ...
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