Historical

SAE AS8860

Name: SAE AS8860 PDF | Request Standard
SKU: 7adec7810be4

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

Standard by SAE International, 2012-05-03

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SAE AS8860.PDFSecure PDF
SAE AS8860.PDFOnline Access

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Language: English
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Language: English
License Type: Enterprise / Multi User
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About This Item

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 rigidity of their control systems and of their carry-through structures. Requirements for wheels, tires, and brakes as they affect air vehicle ground loads are also included. 2 The strength of structures integral with the airplane provided for transmitting catapulting forces to the airplanes, and for engaging shipboard and shore-based arresting gear, and barricades. 3 The strength of anchor-line clamps, and the airplane strength for hoisting, jacking, towing, tie-down, and other ground- or deck-handling conditions. 4 Structural design, analysis, and test data. 5 Laboratory and flight tests performed to obtain information regarding strength rigidity and loads. 6 Definitions. b Landing and Ground Handling Loads c Ground Loads for Navy Acquired Airplanes d Miscellaneous Loads e Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance AS8860 has been reaffirmed to comply with the SAE five-year review policy.

SKU: 7adec7810be4

Publication Date: 2012-05-03

Standard Status: historical

Publisher: SAE International

Document Type: Aerospace Standard

Subject: Landing gear, Military vehicles and equipment, Entry, descent, and landing, Fixed-wing aircraft, Center of gravity (CG), Aerodynamics, Aircraft, Titanium alloys, Roll

Official SAE: Doi link

New Version Available: AS8860B (2023-12-01)
Previous Version: AS8860A (2012-10-03)
This Version: AS8860 (2012-05-03)

Please request information about the document. Contact Page

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