SAE AS8860A-2012
Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
- Standard No.
- SAE AS8860A-2012
- Release Date
- 2012
- Published By
- Society of Automotive Engineers (SAE)
- Status
- Replace By
- SAE AS8860B-2023
- Latest
- SAE AS8860B-2023
- Scope
- This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification contains landing gear strength and rigidity requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing piloted airplanes. These requirements include, but are not limited to the following. a. General Specifications; 1. The shock-absorption characteristics and strength of landing-gear units and the strength and
SAE AS8860A-2012 history
- 2023 SAE AS8860B-2023 Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
- 2012 SAE AS8860A-2012 Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
- 2012 SAE AS8860-2012 Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
- 2006 SAE AS8860-2006 Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
