SGS 1-35 Schweizer   

General Details
Manufacturer: Schweizer
Plane Name:

SGS 1-35

Classified as: Unclassified
Country Of Origin: U S A
Designer: Leslie Schweizer
No. of Seats 1
No. Built 101
L/DMax: 38 88 kph / 48 kt / 55 mph
MinSink: 0.61 m/s / 2.0 fps / 1.18 kt


Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
kg lb.
15 49.2 9.64 103.8 181 400 118 260 299 660 31 8.96 0 0
Aspect ratio: 23.29
Airfoil: Wortmann FX 67-K-170/150
Structure: all-metal monocoque fuselage and single-spar, multi-stringer stressed skin wing; elevator and rudder fabric covered

The 1-35 was designed to 15 m. racing class rules; however it was not fully competitive with its glass fiber contemporaries. The 1-35 was produced in successive, slightly differing, models. The retractable gear versions carry up to 145 kg./ 320 lb. Of water ballast while the 1- 35C had a fixed gear and no provision for ballast. All use flaps for performance and approach control with –8 to +32 degrees for the former, and up to 82 degrees for the latter. Specifications are for the 1-35C. The first 1-35 serial 001, belongs to the National Soaring Museum. ATC.


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