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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 ...
The prop sync should be disengaged when the pilot selects a new propeller r.p.m., then re-engaged after the new r.p.m. is set. The prop sync should always be off for takeoff, landing, and single-engine operation. The AFM/POH should be consulted for system description and limitations.
The Piper PA-23, named Apache and later Aztec, is an American four- to six-seat twin-engined light aircraft aimed at the general aviation market. The United States Navy and military forces in other countries also used it in small numbers.
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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.
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The Continental IO-360 is a family of fuel-injected air-cooled, horizontally opposed six-cylinder aircraft engines manufactured by Continental Motors in the United States of America, now part of AVIC International since 2010.