Dynamic Tests of General Aviation Occupant Restraint Systems

720325

02/01/1972

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
A series of 22 dynamic tests was conducted on general aviation occupant restraint systems. These tests utilized lap belt, and lap belt/shoulder harness restraint systems. With the exception of general aviation aircraft type certificated after September 1969, the Federal Aviation Regulations require only lap belt restraint systems for emergency landing conditions. Based on the longitudinal deceleration/time response of anthropomorphic dummy occupants, it was demonstrated that the lap belt/shoulder harness restraint systems offered occupants successful restraint at occupant inertia force levels substantially above the current regulatory level. The tests, preliminary in nature, warranted continuation of the test program, in that the lap belt/shoulder harness restraint systems showed promise for regulatory inclusion, by virtue of the fact that results were achieved with restraint systems offered as options in recent years, requiring minimal weight increase with fuselage reinforcement adaptable to retrofit as well as new assembly.
Meta TagsDetails
DOI
https://doi.org/10.4271/720325
Pages
16
Citation
Daiutolo, H., "Dynamic Tests of General Aviation Occupant Restraint Systems," SAE Technical Paper 720325, 1972, https://doi.org/10.4271/720325.
Additional Details
Publisher
Published
Feb 1, 1972
Product Code
720325
Content Type
Technical Paper
Language
English