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.
Rationale: This document has been declared "Stabilized" by SAE A-5B, Gears, Struts and Couplings Committee and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability of technical requirements. Newer technology may exist.