STRUCTURAL DESIGN LOADS (SECTION IV - WING)

Grumman Aircraft Engineering, Bethpage, NY

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Luhrssen, R

One section of a 12 part report

A - Effect of Increased RGW to 56,500 LB (2 October 1967)|B - Wing Gust Loads (3 February 1977)|C - Effect of Increased RGW to 58,000 LB (14 October 1967)|D - Effect of Increased RGW to 60,000 LB (4 October 1968)|E - Effect of Increased RGW to 62,500 LB (24 November 1969)|F - Design Loads not Covered In Appendix M, Section II for 65,300 LB RGW (4 February 1977)

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