Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications

Standard:
Reaffirmed:
  • 2012-05-03
 
  • HISTORICAL Access the latest revision: AS8860A
Publisher:
  • SAE International
Pages:
65
Scope:

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:

AS8860 has been reaffirmed to comply with the SAE five-year review policy.

History:
Standard Published Revision Status
AS8860A 2012-10-03 Latest Stabilized
2012-05-03 Historical Reaffirmed
AKA:
  • SAE AS 8860
Sector:
Topic:
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