This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
- Aerospace Standard
Published May 03, 2012 by SAE International in United States
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.
AS8860 has been reaffirmed to comply with the SAE five-year review policy.
|Technical Paper||Landing Gear Integration in an Industrial Multi-Disciplinary Optimization Environment|
|Technical Paper||MANUFACTURING REQUIREMENTS FOR PRODUCING THE MODERN LANDING GEAR|
Data Sets - Support Documents
No Datasets Available
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.