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SAE AS6053A : 2012

Tests, Impact, Shock Absorber Landing Gear, Aircraft

Standard Details

This specification covers definition of landing impact tests which are to be conducted on landing gear assemblies including shock absorbers, suggested instrumentation for the tests and required data of the resulting test report. It is intended to standardize impact test procedures on landing gear shock absorbers and to provide sufficient data to allow evaluation of the design with respect to requirements of MIL-L-8552 and MIL-S-8959 as applicable.

Cross Reference: MIL-A-8860,MIL-A-8863,MIL-A-8868,MIL-L-8552,MIL-S-8698,MIL-S-8959,MIL-STD-831

General Information

Status : Stabilized
Standard Type: Main
Document No: SAE AS6053A : 2012
Document Year: 2012
Pages: 17

Life Cycle

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Stabilized
SAE AS6053A : 2012
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