Piper PA-34-220T Seneca V

Country: Slovakia
Operator: University of Žilina
web page: https://www.lvvc.uniza.sk/sk/
Total lenght: 8,7 m
Wingspan: 11,9 m
Main rotor diameter: 0
Height: 3 m
Maximum take-off weight: 2 125 kg
Ceiling: 7 620 m
Range: 1 640 km
Maximum speed : 377 km/h

The Piper PA-34 220T Seneca aircraft is a six-seater, twin-engine, all-metal, cantilever, low-wing monoplane with a three-point retractable landing gear. It is powered by two six-cylinder turbocharged Teledyne Continental engines of the TSIO-360 series, each with a maximum take-off power of 165 kW / 220 hp and a three-bladed propeller with a constant speed McCauley propeller. It is manufactured by Piper Aircraft Corporation, founded in 1937 in the United States. The production of the type takes place from 1971 to the present. Gradually, it replaced the five main versions, differing in on-board equipment, gradual improvements to the propulsion units and the associated improvements in flight performance and increases in take-off weights.


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