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Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
- Aerospace Standard
Published October 03, 2012 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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:
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.
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.
The strength of anchor-line clamps, and the airplane strength for hoisting, jacking, towing, tie-down, and other ground- or deck-handling conditions.
Structural design, analysis, and test data.
Laboratory and flight tests performed to obtain information regarding strength rigidity and loads.
Landing and Ground Handling Loads
Ground Loads for Navy Acquired Airplanes
Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance
This document has been declared "Stabilized" by SAE A-5B, Gears, Struts and Couplings Committee and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability of technical requirements. Newer technology may exist.
|Technical Paper||AIRCRAFT RADIATORS|
|Technical Paper||Brake System Design for Medium/Heavy Trucks to Meet FMVSS 105-75 Stopping Distance Requirements|
|Technical Paper||Observations and Analyses of Natural Laminar Flow over a Nonlifting Airframe Surface|
Data Sets - Support Documents
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|TABLE 1||Symmetrical Flight Parameters ( )|
|TABLE 2||Design Limit-Sinking Speed ( )|
|TABLE 3||Symmetrical Landing Attitudes ( )|
|TABLE 4||Towing Conditions ( and )|
|TABLE 5||Jacking Loads ( and )|
|TABLE 6||Variation of Landing Impact Conditions|
|TABLE 7||Distribution of Sinking Speeds per 1000 Landings|
|TABLE 8||Number of Times per Thousand Runway Landings that Load Factor n is Experienced|
|TABLE 9||Visual Inspection Criteria|
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