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Full Description

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.
 

Document History

  1. SAE AS6053A


    Tests, Impact, Shock Absorber Landing Gear, Aircraft (Stabilized: Oct 2012)

    • Most Recent
  2. SAE AS 6053

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    Tests, Impact, Shock Absorber Landing Gear, Aircraft ( Reaffirmed: Dec 2007 )

    • Historical Version