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The Pilatus SB-5 was a civil utility aircraft developed by the newly formed Pilatus Aircraft during World War II.

SB-5
A model of the proposed SB-5
Role Civil utility aircraft
National origin Switzerland
Manufacturer Pilatus Aircraft
Developed from Pilatus SB-2 Pelican

Design and development


In the winter of 1941, the construction of the Pilatus SB-2 Pelican began, designed as a low-speed aircraft with STOL (Short Take-Off and Landing) performance, as well as very good climbing performance required for use in narrow alpine valleys. The Pilatus SB-5 was a project for an enlarged version of the Pilatus SB-2,[1] but with the end of WWII the market for light utility transports disappeared so Pilatus abandoned the SB-5 before construction of a prototype began.

The SB-5 was a single-engine high wing monoplane with a fixed nosewheel with a light-alloy semi-monocoque fuselage shell, accommodating 9-10 passengers in 3 rows of three, with an optional passenger in the co-pilot seat. Power was to have been supplied by a Wright Cyclone driving an Escher-Wyss constant-speed reversible pitch 3-bladed propeller.[citation needed]


Specifications (SB-5)


Data from [citation needed]

General characteristics

Performance


References


  1. Gross, Kuno (2019). Pilatus SB-2 Pelican Das Schweizer Bergflugzeug 1938–1949 (in German) (1. Auflage ed.). Studienbüro für Spezialflugzeuge. ISBN 978-3-7494-3640-8.

Further reading





На других языках


[de] Pilatus SB-5

Die Pilatus SB-5 war ein Entwicklungsprojekt aus dem Jahr 1944 der Schweizer Firma Pilatus Flugzeugwerke AG und der ETH Zürich, von dem aber kein Flugzeug gebaut wurde. Der Name Pilatus SB-5 setzt sich zusammen aus dem Herstellerwerk des Flugzeuges, der Pilatus Flugzeugwerke, das Kürzel SB steht für Schweizer Bergflugzeug.
- [en] Pilatus SB-5



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