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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]
The present article gives example specifications for a 1964 PA-28-140. Wow, that's old. There aren't too many of those still flying. Somebody should replace these with specs from something newer. Fogden 14:00, 10 April 2020 (UTC) Actually there are lots from that model year still flying.
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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This page was last edited on 29 September 2011, at 22:12 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may apply.