The purposes of the project reported herein were (1) to establish background for dynamic test criteria for the type certification of aircraft seats and restraint devices, (2) to determine test methods which demonstrate compliance with the dynamic criteria, (3) to express the present static test load requirements for aircraft seats and restraint devices specified in the Federal Aviation Regulations (FAR) in terms of the dynamic criteria, and (4) to relate the static test load requirements to an actual crash environment utilizing the dynamic criteria. (Author)


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