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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.
Data from Jane's all the World's Aircraft 1988–89 General characteristics Crew: 1 or 2 Capacity: 4 or 5 pax + optional seventh seat Length: 8.72 m (28 ft 7 in) Wingspan: 11.86 m (38 ft 11 in) Height: 3.02 m (9 ft 11 in) Wing area: 19.18 m 2 (206.5 sq ft) Airfoil: NACA 65 2 -415 Empty weight: 1,290 kg (2,844 lb) Gross weight: 1,810 kg (3,990 lb) (Max zero fuel weight) Max takeoff weight ...
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 ...
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: 1973 938 Single-engined agricultural monoplane PA-37 0 Proposed twin-engined PA-33 PA-38 Tomahawk: 1978 2,519
Piper PA-34 Seneca: 1: 0: PA-34-220T: Total 14 14 A British Aerospace Jetstream at Cambridge Bay Airport. Previously operated include: [8] Piper Aerostar; Beechcraft ...
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Its construction is partly based upon the twin-engine PZL M-20 Mewa utility plane (Piper PA-34 Seneca II, built under licence in WSK-Mielec). It shares the vertical stabilizer, rudder and main landing gear with the Mewa, while the wings and tail part of fuselage are unified to some degree.