SAE AS 8860A-2012
MIL-886X系列规格中所列的起落架结构要求

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

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标准号

SAE AS 8860A-2012

发布日期

2012年10月03日

实施日期

废止日期

无

国际标准分类号

49.045

发布单位

US-SAE

引用标准

ANSI y 10.7 SAE AMS QQ-A-367 MIL-A-8860 MIL-A-8863 MIL-A-8865 MIL-A-8866 MIL-A-8867 MIL-A-8868 MIL-A-8869 MIL-A-8870 MIL-A-18717 MIL-A-21180 MIL-A-22771 MIL-D-8706 MIL-D-8707 MIL-D-8860 MIL-F-7190 MIL-F-83142 MIL-HDBK-5 MIL-HDBK-17 MIL-HDBK-23 MIL-L-22589

被代替标准

SAE AS 8860-2012

适用范围

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. 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. a. General Specifications; 1. The shock-absorption characteristics and strength of landing-gear units and the strength and