Pilatus SB-2. The Pilatus SB-2 Pelican was a civil utility aircraft developed by a purposely founded development bureau at the ETH Zurich on behalf of the Federal Air Authority. In November 1940 it was decided to go on with the project and build the aircraft, in February 1941 the Authority approved the development bureau to have it built at the newly formed Pilatus Aircraft company.

Design and development
In 1938 the Federal Air Authority was looking for an aircraft able to land at minial airfields in mountain valleys. In fact the aircraft was desired to define the criteria such possible future airfields would have to meet. So this was not to be the aircraft for such air transport itself but a means to find possible airfield locations.

The previous project of a four-seater STOL experimental aircraft under the designation Studienbüro für Spezialflugzeuge SB-1 was not implemented, so it was followed by the SB-2, which at some moments was also discussed for commercial use.
Work on the SB-2 Pelican, a special “slow-flying” aircraft, commenced in the winter of 1941. Good short takeoff and landing credentials, plus steep climbing capabilities, were essential attributes of the aircraft flown in the narrow Alpine valleys at that time. The aircraft was designed to carry five people, the double controls could be reduced to one if flown with only one pilot.

The configuration of the SB-2 was slightly unusual, in that it was provided with tricycle undercarriage (an uncommon feature at the time), and a wing that had a slight forward sweep.

As it turned out, the type was never actually tested in its originally intended role. Only twice the aircraft was used later by the company it was sold to, Alpar, to land in a narrow mountain valley.

The SB-2 also served as the basis for the design work on a larger STOL aircraft with an increased passenger capacity, the Studienbüro für Spezialflugzeuge SB-5, whose development was stopped prior to any construction work.

Operational history
The SB-2 made its maiden flight on 30 May 1944. After extensive trials, the only model built went to Alpar AG in Bern. The Pelikan was well suited for passenger operations, but could have also been used for aerial photography, which it never was. The bottom loading opening was useful for some freight transport and agricultural work.

During an air display on 13 June 1948, the Pelican flipped over because the nosewheel sheared off from an unnoticed transverse slip. It was stored damaged during which time still improvements were discussed by the chief engineer Belart of the Studienbüro, while Alpar was hoping to raise the takeoff weight and asked Pilatus to submit a bid for a conversion to seven seats at the end of January 1949. Calculations were made and drawings produced with other wheels. When Pilatus refused to offer a price and insisted on effort calculation, estimated at 160'000 Swiss Francs, Alpar had to give up plans to rebuild the aircraft. On March 23, 1949, the aircraft was removed from the Swiss registry.

Specifications (SB-2)

See also

Further reading
Pilatus SB-2 Pelican Das Schweizer Bergflugzeug 1938–1949, Studienbüro für Spezialflugzeuge, Kuno Gross, .

References

1940s Swiss civil utility aircraft
High-wing aircraft
Single-engined tractor aircraft
SB-2
Forward-swept-wing aircraft
Aircraft first flown in 1944
Aircraft with fixed tricycle landing gear
ETH Zurich
Single-engined piston aircraft