Pilatus PC-10

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PC-10
Role light transport
National origin Switzerland
Manufacturer Pilatus Aircraft
First flight non
Number built 0

The Pilatus PC-10 was the common name of different designs for a twin-engine aircraft manufacturer Pilatus Aircraft, but none of them reached the production stage.

Turbopropversion PC-8D / PC-10 Twin Porter[edit]

Pilatus PC-8D

The first draft was basically an unchanged Pilatus PC-8D Twin Porter, the place of the piston engines would have been equipped with turboprop.

PC-10 Mini Twin[edit]

Under the name PC-10 MiniTwin a machine was designed for 11 people, on the left rear side of the hull with a cargo door with integrated passenger door. The aircraft had. A projected total length of 11.44 m and a height of 4.75 m with a span of 16 m.

Twin Project PC-10[edit]

Under the name Twin Project PC-10 is a slightly larger plane was designed which possessed on the left rear fuselage just a passenger sliding door that opens to the rear. For it in the rear fuselage a loading door was built. The aircraft would have a total length of 13.50 m, a height of 6.08 meters and a wingspan of 19 meters. The machine should be able to transport 16 people, or nearly 2 tons of cargo. It had been equipped with a fixed landing gear and two Garrett TPE-331 or Pratt & Whitney PT6A-27 turboprop engines. Externally, the latter two designs regarding chassis, wings and engine assembly resembled strongly the DHC-6 Twin Otter, but the tailplane difference to an enlarged version of the Pilatus PC-6 and Pilatus PC -8 Twin Porter used that has no sweep. Development of the PC-10 was later transferred to Poligrat but little progress was made.[1]

PC-10 Masterporter[edit]

The PC-10 Masterporter was a project for a military cargo plane. Designed as a high-decker with two turbopropturbines, with a two-man cockpit, retractable landing gear and rear loading ramp. The size and design of the PC-10 Masterporter would have roughly corresponded to the CASA C-212. Since the demand for such an aircraft in the Swiss Air Force as a launch costumer could not assert itself, the project was terminated.

References[edit]

  1. ^ Taylor, John W.R., ed. (1975). Jane's all the world's aircraft, 1975-76 (66th annual ed.). New York: Franklin Watts Inc. p. 95. ISBN 978-0531032503.

Further reading[edit]

  • Eichenberger, Roland (1989). Pilatus Flugzeuge: 1939–1989. Stans: Pilatus Flugzeugwerk.

External links[edit]