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SAE AS 8860 : 2012

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS
Available format(s)

Hardcopy , PDF

Superseded date

19-12-2023

Language(s)

English

Published date

03-10-2012

Publisher

SAE International

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

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.

Committee
A-5
DocumentType
Standard
Pages
66
ProductNote
This standard is now stabilized
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

SAE ARP 1311 : 2015 LANDING GEAR STRUCTURES AND MECHANISMS
SAE AIR 5914 : 2014 LANDING GEAR FATIGUE SPECTRUM DEVELOPMENT FOR PART 25 AIRCRAFT
SAE ARP 1595 : 2013(R2019) DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS
SAE ARP1311D:2018(R2023) Landing Gear Structures and Mechanisms

MIL-A-8865 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
MIL HDBK 5 : G_VOL2 METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
MIL-A-8863 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
MIL-STD-2066 Base Document:1981 CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN
MIL-T-81259 Revision B:1991 TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
MIL-A-22771 Revision D:1984 ALUMINUM ALLOY FORGINGS, HEAT TREATED
ANSI Y10.7 : 1954 LETTER SYMBOLS/AERONAUTICAL SCIENCES
MIL-A-8869 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS
MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
QQ-A-367 Revision H:1973 ALUMINUM ALLOY FORGINGS
MIL-STD-2175 Revision A:1993 CASTING, CLASSIFICATION AND INSPECTION OF
MIL-F-7190 Revision B:1985 FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS
MIL-L-22589 Revision D:1991 LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
MIL-A-8868 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
MIL-A-8867 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
MIL-T-6053 Revision C:1977 Tests, Impact, Shock Absorber Landing Gear, Aircraft
MIL-A-21180 Revision D:1984 ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
MIL-A-8861 Revision B:1986 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
MIL-A-8866 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
MIL-A-18717 Revision C:1993 ARRESTING HOOK INSTALLATIONS, AIRCRAFT
MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-F-83142 Revision A:1969 FORGING, TITANIUM ALLOYS, PREMIUM QUALITY
MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR

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Hardcopy - English
PDF - English
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