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SAE International - ARP4915A

Disposition of Landing Gear Components Involved in Accidents/Incidents

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Organization: SAE International
Publication Date: 20 June 2011
Status: active
description:

This document establishes a procedure for disposition of landing gear components that have been involved in accidents/incidents. The recommendations in this document apply to components... View More

Document History

ARP4915A
June 20, 2011
Disposition of Landing Gear Components Involved in Accidents/Incidents
This document establishes a procedure for disposition of landing gear components that have been involved in accidents/incidents. The recommendations in this document apply to components made of...

References

This document references:
AMS2658 - HARDNESS AND CONDUCTIVITY INSPECTION OF HEAT TREATED ALUMINUM ALLOY PARTS
Published by SAE International on April 1, 1980
This specification establishes hardness and electrical conductivity acceptance criteria of finished or semi-finished parts of wrought aluminum alloys.
This document references:
AMS2759 - HEAT TREATMENT OF STEEL PARTS General Requirements
Published by SAE International on October 1, 1984
This specification establishes general requirements for the processes listed in 2.1.1 for heat treatment of steel parts (See 8.1.1 ) by users or their vendors or subcontractors.
This document references:
AMS2770 - HEAT TREATMENT OF ALUMINUM AND ALUMINUM-BASE ALLOYS
Published by SAE International on June 1, 1974
This specification covers the engineering requirements for the thermal treatment of aluminum-base alloy parts.
This document references:
AMS2801 - HEAT TREATMENT OF TITANIUM ALLOY PARTS
Published by SAE International on July 1, 1990
This specification covers the engineering requirements for heat treatment by part fabricators (users) or their vendors or subcontractors of parts (See 1.1.2 ) made from the following titanium alloys.
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