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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 Piper PA-23, named Apache and ... Max takeoff weight: 5,200 lb (2,359 kg) Fuel capacity: 140 US gal (120 imp gal; ... Piper PA-34 Seneca; References
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
First model with increased fuel capacity via fuel tanks inside wings and ... Gross weight: 4,600 lb (2,087 kg) Fuel capacity: 100 ... Piper PA-23; Piper PA-34 Seneca;
Piper PA-34 Seneca Cessna O-2 Skymaster Cessna T-41 Mescalero: The Continental IO-360 is a family of fuel-injected air-cooled, ... Dry weight: 294 lb (133 kg) Components.
Gross weight: 3,400 lb (1,542 kg) Fuel capacity: 100 US Gallons (379 L) ... Piper PA-23; Piper PA-34 Seneca; Temco D-16; Related lists. List of civil aircraft; References
Gross weight: 5,150 lb (2,336 kg) Fuel capacity: 153 US gal (127 imp gal; 580 L) (usable capacity) ... Piper Aztec; Piper PA-34 Seneca; References. Notes