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  2. Piper PA-32 Cherokee Six - Wikipedia

    en.wikipedia.org/wiki/Piper_PA-32_Cherokee_Six

    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]

  3. Piper PA-32R - Wikipedia

    en.wikipedia.org/wiki/Piper_PA-32R

    PA-32R-300 (1976–1978) Marketed as the Piper Cherokee Lance.Initial version of the retractable PA-32 line, with a standard tail. [4]PA-32RT-300 (1978–1979) After the first half of 1978, Piper modified the tail to a "T" design with the stabilator (horizontal stabilizer/elevator) moved to the top of the vertical tail.

  4. List of Piper models - Wikipedia

    en.wikipedia.org/wiki/List_of_Piper_models

    PA-32 Cherokee Six: 1966 4,373 Six-seat Cherokee derivative with wider cabin PA-32R Lance/Saratoga: 1976 2,721 Retractable landing gear variant of the PA-32 PA-33 Comanche: 1966 1 Pressurized Comanche PA-34 Seneca: 1972 5,000+ Twin-engine derivative of PA-32R PA-35 Pocono: 1968 1 Twin-engined pressurized commuter airliner PA-36 Pawnee Brave ...

  5. File:Piper.pa32.cherokee.six.g-bxwp.arp.jpg - Wikipedia

    en.wikipedia.org/wiki/File:Piper.pa32.cherokee...

    Piper PA-32-300 Cherokee Six (UK registration G-BXWP) at Kemble Airfield, Gloucestershire, England. Built 1973. Photographed by Adrian Pingstone in July 2005 and released to the public domain.

  6. Piper PA-28 Cherokee - Wikipedia

    en.wikipedia.org/wiki/Piper_PA-28_Cherokee

    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.

  7. Lycoming O-320 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-320

    150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as A2A but with straight riser in oil sump and -32 carburetor. [4] O-320-A2C 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as A2B but with retard breaker magnetos. [4] O-320-A2D

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  9. Piper PA-31 Navajo - Wikipedia

    en.wikipedia.org/wiki/Piper_PA-31_Navajo

    The PA-31-300 was certified by the FAA in June 1967, the only variant without turbocharged engines: 300 hp (224 kW) Lycoming IO-540-M1A5 engines driving two-bladed propellers. [8] Unofficially, the initial model was referred to as the PA-31-310. Only 14 PA-31-300 were built in 1968 and 1969: the smallest variant production. [2] [9]