Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
|
Product Code: AS8860
Date Published: 2006-04-25
Issuing Committee:
A-5b Gears, Struts And Couplings Committee
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.
Product Status: In Stock
File Size:
2526K
Purchase more aerospace standards and aerospace material specifications and save!
AeroPaks offers a customized subscription plan that lets you pay
for just the documents that you need, when you need them.
Learn more >
| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| AS8860 |
2006-04-25 |
Issued |
|
Related Content
|
