Schweizer SGS 1-35 - Development

Development

Schweizer Aircraft started construction of the 1-35 prototype in late 1972 and it first flew in April 1973. The company carried out side-by-side comparisons with fiberglass sailplanes as part of 50 hours of flight evaluations before making the decision to proceed with manufacturing the design on 10 May 1973.

The 1-35 is an all-metal aircraft with a monocoque fuselage. The wing has a single spar and the stressed skin features multi-stringers for stiffness, to best retain airfoil shape and laminar flow. The aircraft's elevator and rudder are fabric covered. The 1-35 carries 320 lb (145 kg) of water ballast in two wing tanks.

Because the 15 Metre Class allows flaps, the SGS 1-35 is equipped with plain flaps that can be selected from −8 to +32 degrees for soaring and inter-thermal speed and +32 to +82 degrees for landing.

The 1-35 received type certificate G4EA on 25 April 1974.

The type certificate is currently held by K & L Soaring of Cayuta, New York. K & L Soaring now provides all parts and support for the Schweizer line of sailplanes.

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