The Piper PA-35 Pocono was an American 16 or 18 seat commuter airliner that Piper developed in the late 1960s. Design work began in 1965 for a twin-engined piston non-pressurized airliner, and the single prototype first flew on 13 May 1968. It was a low-wing monoplane planned around two Lycoming TIO-720 piston engines, later uprated to 520 horsepower, with a larger tail and a stretched fuselage after development problems. Development stopped in 1969 for lack of a suitable engine and because several small regional airlines were failing. Later turboprop and four-engine proposals were not built, and a fuselage was sent to Poland around 1978 for the abandoned M-19 programme.
Facts
Engine Class Top Speed (km/h) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Piper PA-35 Pocono (Wikipedia)
Of Make
Source Piper PA-35 Pocono (Wikipedia)
Sources
1. Piper PA-35 Pocono (Wikipedia)
Design and development, prototype first flight
the prototype first flew on 13 May 1968
Design and development, end of programme
Development was stopped in 1969
Lead, number built
Only one aircraft was built
Design and development, intended powerplant
twin-engined piston non-pressurized commuter airliner
Lead
was an American 16/18 seat commuter airliner
Specifications (1969 variant), empty weight
Empty weight: 5,572 lb (2,527 kg)
Specifications (1969 variant), maximum speed
Maximum speed: 260 mph (417 km/h, 230 kn)
Lead, manufacturer
commuter airliner developed by Piper in the late 1960s
Lead, country of origin
was an American 16/18 seat commuter airliner developed by Piper
Of Make: Piper Aircraft, Lead, make
commuter airliner developed by Piper in the late 1960s
In Group: Twin-Engine and Turboprop Utility Aircraft, Lead, group placement
twin-engined piston non-pressurized commuter airliner
Exemplifies: General Aviation, Lead, mode placement
commuter airliner developed by Piper in the late 1960s
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