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SAE AS 8860A:2012-10-03
Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications (Stabilized: Oct 2012)More info
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. These requirements include, but are not limited to the following:
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2012-05-01 |
| ICS | 49.045 : Structure and structure elements |
| Number of pages | 66 |
| Replace | SAE AS 8860:2012-05-03 |
| Set | AEROPAKS10U-10 |
| Year | 2012 |
| Document history | SAE AS 8860:2012-05-03 |
| Country | USA |
| Keyword | SAE 8860;SAE AS8860A;SAE AS8860A;SAE AS 8860 |