Glasair I and II Wing Analysis SH-200

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• Create Date December 11, 2018
• Last Updated December 11, 2018

Covers models SH-2, SH-2F, SH-2R
Prepared by R.M. Gavinsky, Stoddard-Hamilton, October 6, 1987

Scope: The purpose of this analysis is to check the stress levels in the main and rear spar caps due to wing bending, and to see whether the ultimate loads exceed the allowables.

This document may be required by some European jurisdictions for the purpose of registering a Glasair aircraft. (France, Switzerland)

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