STRUCTURAL DESIGN LOADS (SECTION V - HORIZONTAL TAIL LOADS)

Grumman Aircraft Engineering, Bethpage, NY

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Pittel, M

One section of a 12 part report

A - Effect of Increased RGW to 56,500 LB (2 October 1967)|B - Effect of Increased RGW to 58,000 LB (14 October 1967)|C - Effect of Increased RGW to 60,000 LB (1 Auguat 1968)|D - Effect of Increased RGW to 62,500 LB (8 December 1969)

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