Static Test Procedures for Restraint Anchorages in Small Aircraft
Date Published: 1987-05-01
Paper Number:871007
DOI: 10.4271/871007
Citation:
Gowdy, V., Rathgeber, R., and Ross, J., "Static Test Procedures for Restraint Anchorages in Small Aircraft," SAE Technical Paper 871007, 1987, doi:10.4271/871007.
Author(s):
Van Gowdy - FAA Civil Aeromedical Institute
Ronald K. Rathgeber - FAA Central Region Certification Div.
James W. Ross - FAA Aviation Standards National Field Office
Abstract:
Recent amendments to the Federal Aviation Regulations (FAR) increase the requirements for installation and utilization of shoulder harnesses in small airplanes which are certificated in the normal, utility, or aerobatic category. Static testing of a combined lap belt and shoulder harness in a manner which produces a predictable load distribution to the anchorage points can be difficult. A series of tests were performed by the Federal Aviation Administration (FAA) Civil Aeromedical Institute (CAMI) to evaluate static test procedures for restraint anchorages on small airplane forward facing seats that have a lap belt and shoulder harness anchored to the airframe.
File Size: 399K
Product Status: In Stock
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