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Twin-engine derivative of PA-32R PA-35 Pocono: 1968 1 Twin-engined pressurized commuter airliner PA-36 Pawnee Brave: 1973 938 Single-engined agricultural monoplane PA-37 0 Proposed twin-engined PA-33 PA-38 Tomahawk: 1978 2,519 Two-seat basic trainer PA-39 Twin Comanche C/R: 1970 155 Improved PA-30 with counter-rotating propellers: PA-40 Arapaho ...
The Piper PA-34 Seneca is a twin-engined light aircraft, produced in the United States by Piper Aircraft.It has been in non-continuous production since 1971. [4] [5] [6] The Seneca is primarily used for personal and business flying [1] as well as multi-engine class rating flight training.
The last 43 of the order were completed as required by Glenn Martin. All these aircraft became the Maryland Mk.I. A further 150 aircraft had been ordered directly by Britain with two-speed superchargers on their Twin Wasps as the Maryland Mk.II. [1] Many of the aircraft were shipped to Egypt and Malta in time for the 1941 fighting there.
The Piper PA-30 Twin Comanche was designed as a twin-engined variant of the Piper PA-24 Comanche.A complex light twin, with retractable landing gear, seating 4 (in original models) to 6 (in later models), and cruise speeds ranging from 160–210 mph on twin 160 horsepower engines, it competed with the more-powerful Cessna 310 and Beech Baron, and later with Piper's other light twins.
Piper PA-44-180 Seminole PA-44 landing Piper PA-44-180 Seminole. The Piper PA-44 Seminole is an American twin-engined light aircraft manufactured by Piper Aircraft. [2] The PA-44 is a development of the Piper Cherokee single-engined aircraft and is primarily used for multi-engined flight training. [2] [3]
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The PA-31 series was manufactured under licence in several countries from kits of parts supplied by Piper. [20] [21] Chincul SACAIFI in Argentina assembled most of the series as the PA-A-31, PA-A-31-325, PA-A-31P and PA-A-31-350 and Aero Industrial Colombiana SA (AICSA) in Colombia assembled PA-31, PA-31-325 and PA-31-350 aircraft. [22]
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.