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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.
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-34-200T Seneca 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-32RT-300T Turbo Lance II Piper PA-44 ...
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.
160 hp (119 kW) at 2700 rpm, Minimum fuel grade 100/130 or 91/96 avgas, compression ratio 8.50:1. Same as B1A but with straight riser in oil sump and -32 carburetor. [4] O-320-B2A 160 hp (119 kW) at 2700 rpm, Minimum fuel grade 100/130 or 91/96 avgas, compression ratio 8.50:1. Same as B1A but with fixed-pitch propeller provisions. [4] O-320-B2B
The main petroleum component used in blending avgas is alkylate, which is a mixture of various isooctanes. Some refineries also use reformate.All grades of avgas that meet CAN 2–3 [further explanation needed], 25-M82 [further explanation needed] have a density of 6.01 pounds per US gallon (720 g/L) at 15 °C (59 °F).
The PA-32 series was developed to meet a requirement for a larger aircraft than the four-seat Piper PA-28 Cherokee. [3] The first prototype PA-32 made its initial flight on December 6, 1963, with the type being publicly announced in October 1964, with Federal Aviation Administration (FAA) aircraft_type certification following on March 4, 1965. [4]
The standard fuel capacity of the PA-24-180 was 60 US gallons (230 L). The flaps were manually actuated, controlled by the same Johnson bar actuator as the Piper Cherokee. The aircraft specifications were for cruise speeds of 116 to 139 knots (215 to 257 km/h) and fuel burns between 7.5 and 10.5 gallons per hour (28 and 40 L/h) at 55 and 75% ...
PA-28 may refer to: Pennsylvania's 28th congressional district; Pennsylvania Route 28, a highway; Piper PA-28 Cherokee light aircraft This page was last edited on ...