SAE AS8860A
Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications(STABILIZED Oct 2012)
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.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AS8860A | 2012-10-03 | Latest | |
| AS8860 | 2006-04-25 | Historical |