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SAE ARP 1311 : 2015

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 STRUCTURES AND MECHANISMS
Available format(s)

Hardcopy , PDF

Superseded date

06-11-2018

Language(s)

English

Published date

01-01-2015

1. SCOPE
2. APPLICABLE DOCUMENTS
3. DESIGN REQUIREMENTS
4. DESIGN VERIFICATION
5. NOTES

Pertains to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil and military aircraft.

Committee
A-5B
DevelopmentNote
Supersedes SAE AIR 1494. (04/2010)
DocumentType
Standard
Pages
32
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

SAE AIR 5552 : 2015 DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS
SAE ARP 5908 : 2013 LANDING GEAR SERVICING
SAE AIR 5883 : 2012 LANDING GEARS SHOCK STRUTS BEARING SELECTION

SAE AS 4716 : 2011 GLAND DESIGN, O-RING AND OTHER SEALS
SAE AIR 1752 : 2013 AIRCRAFT NOSEWHEEL STEERING/CENTERING SYSTEMS
FAA AC 23-13 : 2005 FATIGUE, FAIL-SAFE, AND DAMAGE TOLERANCE EVALUATION OF METALLIC STRUCTURE FOR NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES
MMPDS 03 : 2006 METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS)
SAE AIR 1594 : 2010 PLAIN BEARING SELECTION FOR LANDING GEAR APPLICATIONS
SAE AMS QQ C 320 : 2000 CHROMIUM PLATING (ELECTRODEPOSITED)
MIL-A-8863 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
SAE AS 6053 : 2012 TESTS, IMPACT, SHOCK ABSORBER LANDING GEAR, AIRCRAFT
SAE AIR 4566 : 2015 CRASHWORTHY LANDING GEAR DESIGN
MS33675 Revision C:1971 SCRAPER, INSTALLATION, PACKING GLAND RING
MIL-T-81259 Revision B:1991 TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
MIL-PRF-5606 Revision H:2002 HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE
SAE AIR 5883 : 2012 LANDING GEARS SHOCK STRUTS BEARING SELECTION
SAE ARP 4912 : 2013 DESIGN RECOMMENDATIONS FOR SPARE SEALS IN LANDING GEAR SHOCK STRUTS
SAE AMS QQ N 290 : 2015 NICKEL PLATING (ELECTRODEPOSITED)
NAS 1613 : 2002 PACKING, PREFORMED, ETHYLENE PROPYLENE RUBBER
MS15003 Base Document:1951 FITTINGS, LUBRICATION (HYDRAULIC) SURFACE CHECK, 1/8 PIPE THREADS, STEEL TYPE 3
MS33559 Revision E:1989 ADAPTOR, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF
ASME B46.1 : 2009 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
SAE AMS P 83461 : 1998 Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C)
MS28889 Revision L:1987 VALVE, AIR, HIGH PRESSURE CHARGING, 5000 PSI
MIL-PRF-87257 Revision C:2017 HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE
SAE ARP 1595 : 2013(R2019) DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS
MIL A 8862 : 0 AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS
MS15001 Revision A:1959 FITTINGS, LUBRICATION (HYDRAULIC) SURFACE CHECK, 1/4-28 TAPER THREADS, STEEL, TYPE 1
MIL-PRF-5503 Revision G:2013 ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR
MIL-L-22589 Revision D:1991 LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
SAE ARP 5935 : 2013 USE OF HVOF THERMAL SPRAY COATINGS FOR HARD CHROME REPLACEMENT IN LANDING GEAR APPLICATIONS
MIL-L-8552 Revision C:1965 LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE]
MIL-STD-809 Revision B:1986 ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF
FAA AC 25.571-1 : 2011 DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE
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
SAE AS 1241 : 2016 FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT
SAE ARP 5936 : 2016 LANDING GEAR STORAGE
MS33651 Revision C:2014 BOSS AND INSTALLATIONS - AIR CONNECTION
MIL-PRF-83282 Revision D:1997 HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537
SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS
MIL-STD-805 Revision B:1987 TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR
SAE AS 4941 : 2015 AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS
SAE AS 4052 : 2015 GLAND DESIGN: SCRAPER, LANDING GEAR, INSTALLATION
JSSG-2006 Base Document:1998 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
SAE ARP 4915 : 2016 DISPOSITION OF LANDING GEAR COMPONENTS INVOLVED IN ACCIDENTS/INCIDENTS
SAE AIR 5451 : 2016 A GUIDE TO LANDING GEAR SYSTEM INTEGRATION
SAE AIR 5479 : 2007 ENVIRONMENTALLY COMPLIANT PROCESSES FOR LANDING GEAR
SAE ARP 5429 : 2017 LANDING GEAR FATIGUE TESTS WITH EQUIVALENT DAMAGE SPECTRA
MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
SAE AIR 5358 : 2016 LANDING GEAR SHOCK STRUT HYDRAULIC FLUID

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