STRUCTURAL DESIGN LOADS (SECTION VII - FUSELAGE LOADS)

Grumman Aircraft Engineering, Bethpage, NY

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Brodman, H

One section of a 12 part report

A - Effect of Increased RGW to 56,500 LB (27 October 1967)|B - Additional Fuselage Loads (13 October 1967)|C - Effect of Increased RGW to 58,000 LB (14 October 1967)|D - Additional Fuselage Loads (26 February 1968)|E - Effect of Increased RGW to 60,000 LB (4 October 1968)|F - Effect of Increased RGW to 62,500 LB (20 May 1970)

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