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150 hp (112 kW) at 2700 rpm, or 140 hp (104 kW) at 2450 rpm Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as E1A but with fixed-pitch propeller, 3/8 inch attaching bolts and an alternate power rating of 140 hp (104 kW). [4] O-320-E2B 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1.
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.
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 PA-28 PA-28R Arrow: 1967 6,694 Retractable landing gear variant of the PA-28 PA-28R-300 Pillán: 1982 2 [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 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 ...
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Pages for logged out editors learn more. Contributions; Talk; Piper PA-28 Turbo Dakota
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English: A 3-view line drawing of the Piper PA-28-140, PA-28-150, PA-28-160 and PA-28-180 Cherokee or Cherokee B. Identifiable by the oval light retainer assembly in the nose, lack of a fillet on the vertical stabilizer and lack of third window. The width of the light retainer assembly in the profile view and slope on the top of the third ...