T-39 Landing Gear Design Evaluation and Fatigue Analysis. Phase II. Volume 1 of III,
BENDIX CORP SOUTH BEND IND ENERGY CONTROLS DIV
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The purpose of this report is to accomplish a fatigue damage evaluation of the original and revised main and nose landing gears of the North American Rockwell T-39 aircraft. The fatigue loads spectrum utilized in this evaluation is developed by Bendix ECD from flight test data supplied by Hill Air Force Base.
- Training Aircraft