Glasair I and II Wing Analysis SH-200

    Glasair I and II Wing Analysis SH-200
    Login is required to access this page
    • Version
    • Downloads 120
    • File Size 6.33 MB
    • File Count 1
    • 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)

    Attached Files

    Previous articleAmateur-Built Aircraft and Ultralight Flight Testing Handbook AC 90-89B
    Next articleGlasair Landing Gear Hydraulic System Schematic
    Omar Filipovic
    Omar Filipovic is president of the Glasair Aircraft Owners Association as well as the chief tinkerer and content editor for this website. He is also the web editor for Kitplanes Magazine. Omar is building a GlaStar in Portland, Oregon.