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  • SAE ARP 1311 : 2015

    View superseded by
    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    LANDING GEAR STRUCTURES AND MECHANISMS

    Available format(s):  Hardcopy, PDF

    Superseded date:  11-06-2018

    Language(s):  English

    Published date:  01-01-2015

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

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

    Abstract - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Committee A-5B
    Development Note Supersedes SAE AIR 1494. (04/2010)
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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