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1959 Piper PA-24 180. The original version of the Comanche was the PA-24, which featured a carbureted 180 hp (134 kW) Lycoming O-360-A1A engine, swept tail, laminar flow airfoil, and all-flying stabilator. The standard fuel capacity of the PA-24-180 was 60 US gallons (230 L).
Piper PA-24 Comanche, a light aircraft first produced in 1957 Topics referred to by the same term This disambiguation page lists articles associated with the same title formed as a letter–number combination.
PA-25-235 and PA-25-260 Pawnee D The Pawnee D was also powered by a Lycoming O-540 of 260hp but featured fuel tanks fitted in the outer wings and metal covered ailerons and flaps. From 1980 it was known as the PA-25-235 Pawnee. eTug A modified PA-25 powered by a General Motors LS automotive engine driving a three-bladed propeller. [10]
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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.
The prototype PA-23 was a four-seat, low-wing, all-metal monoplane with a twin tail, powered by two 125 hp Lycoming O-290-D piston engines; [1] it first flew on March 2, 1952. [2] The aircraft performed poorly, so it was redesigned with a single vertical stabilizer and an all-metal rear fuselage and more powerful 150 hp Lycoming O-320 -A engines.
Piper started the design work in 1965 for a twin-engined piston non-pressurized commuter airliner and the prototype first flew on 13 May 1968. [1] It was a low-wing monoplane that was intended to be powered by two 475 hp (354 kW) Lycoming TIO-720-B1A piston engines then under development.