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SAE AS 8860 : 2012

SAE AS 8860 : 2012

LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS

SAE International

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Table of Contents

1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES

Abstract

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.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee A-5

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