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Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
- Aerospace Standard
- AS8860
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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
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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.
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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.
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3
The strength of anchor-line clamps, and the airplane strength for hoisting, jacking, towing, tie-down, and other ground- or deck-handling conditions.
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4
Structural design, analysis, and test data.
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5
Laboratory and flight tests performed to obtain information regarding strength rigidity and loads.
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6
Definitions.
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1
-
b
Landing and Ground Handling Loads
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c
Ground Loads for Navy Acquired Airplanes
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d
Miscellaneous Loads
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e
Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance
Rationale
AS8860 has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
| Technical Paper | Landing Gear Integration in an Industrial Multi-Disciplinary Optimization Environment |
| Technical Paper | MANUFACTURING REQUIREMENTS FOR PRODUCING THE MODERN LANDING GEAR |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| 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 |
Issuing Committee
Reference
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