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  • SAE AIR 1594 : 2010

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    PLAIN BEARING SELECTION FOR LANDING GEAR APPLICATIONS

    Available format(s):  Hardcopy, PDF

    Superseded date:  29-04-2018

    Language(s):  English

    Published date:  01-01-2010

    Publisher:  SAE International

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

    1. SCOPE
    2. REFERENCES
    3. PLAIN BEARING CONFIGURATIONS
    4. LANDING GEAR BEARING CONSIDERATION
    5. MATERIAL SELECTION FOR LUBRICATED BEARINGS
    6. WORKING PRESSURES FOR LUBRICATED BEARINGS
    7. INTERFERENCE FITS FOR JOURNAL BEARINGS
    8. BEARING TO PIN CLEARANCES
    9. CORROSION PREVENTION
    10. LUBRICATION
    11. SELF-LUBRICATING BEARINGS
    12. INSTALLATION OF SELF-LUBRICATING BEARINGS
    13. WORKING PRESSURES FOR SELF-LUBRICATING BEARINGS
    14. MATING PIN/SHAFT SURFACE FINISHES
    15. ENVIRONMENTAL CONCERNS
    16. NOTES

    Abstract - (Show below) - (Hide below)

    Aims to provide advisory information for the selection of plain bearings and bearing materials most suitable for aircraft landing gear applications.

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

    Committee A-5B
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By

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

    SAE ARP 1311 : 2015 LANDING GEAR STRUCTURES AND MECHANISMS
    SAE AIR 5883 : 2012 LANDING GEARS SHOCK STRUTS BEARING SELECTION

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

    SAE AMS 4534 : 2013 COPPER-BERYLLIUM ALLOY, BARS AND RODS 98CU - 1.9BE SOLUTION HEAT TREATED, COLD WORKED, AND PRECIPITATION HEAT TREATED (TH04, FORMERLY HT)
    SAE AS 14103 : 2010 BEARING, PLAIN, SELF-LUBRICATING, SELF-ALIGNING, LOW SPEED, WIDE, GROOVED RACE, -65 TO +325 DEGREES F
    SAE AS 81934 1 : 2004 BEARING, SLEEVE, PLAIN, SELF-LUBRICATING, -65 TO 325 DEGREE F
    SAE AMS 4598 : 2012 COPPER NICKEL TIN ALLOY, MECHANICAL TUBE, 77CU - 15NI - 8SN, SOLUTION ANNEALED AND SPINODAL HARDENED (TX 00)
    SAE AMS 4596E:2010(R2018) COPPER NICKEL TIN ALLOY, BARS AND RODS, 77CU - 15NI - 8SN, SOLUTION ANNEALED AND SPINODAL HARDENED (TX 00)
    SAE AS 81820 : 2014 BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION
    SAE AMS 4881 : D2012(R2018) NICKEL-ALUMINUM-BRONZE, MARTENSITIC, SAND, CENTRIFUGAL AND CONTINUOUS CASTINGS, 78CU - 11AL - 5.1NI - 4.8FE, QUENCH HARDENED AND TEMPER ANNEALED
    MIL PRF 81733 : D SEALING AND COATING COMPOUND, CORROSION INHIBITIVE
    MIL PRF 32014 : A GREASE, AIRCRAFT AND INSTRUMENT
    SAE AS 81936 : 2006 BEARINGS, PLAIN, SELF-ALIGNING (CU-BE BALL, CRES RACE) GENERAL SPECIFICATION FOR
    SAE AMS 4880 : 2005 ALUMINUM BRONZE ALLOY, CENTRIFUGAL AND CONTINUOUS-CAST CASTINGS - 81.5CU - 10.3AL - 5.0NI - 2.8FE QUENCH HARDENED AND TEMPER ANNEALED (TQ50)
    SAE AIR 5883 : 2012 LANDING GEARS SHOCK STRUTS BEARING SELECTION
    SAE AMS 5643 : 2016 STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE
    MIL B 8942 : A BEARINGS, PLAIN, TFE LINED, SELF-ALIGNING
    SAE AMS 4590 : 2015 EXTRUSIONS, NICKEL-ALUMINUM BRONZE, MARTENSITIC, 78.5CU - 10.5AL - 5.1NI - 4.8FE, QUENCHED AND TEMPERED (TQ50)
    SAE AS 21230 : 2012 BEARING, PLAIN, SELF-ALIGNING, GROOVED OUTER RINGER PTFE LINED, WIDE
    SAE AMS 4533 : 2013 COPPER-BERYLLIUM ALLOY, BARS AND RODS, 98CU - 1.9BE, SOLUTION AND PRECIPITATION HEAT TREATED (TF00, FORMERLY AT)
    SAE AMS 4597 : 2011 COPPER-NICKEL-TIN ALLOY, BARS AND RODS, 77CU - 15NI - 8SN, SOLUTION ANNEALED, COLD FINISHED AND SPINODAL HARDENED (TX TS)
    SAE AS 81934 : 2016 BEARINGS, SLEEVE, PLAIN AND FLANGED, SELF-LUBRICATING
    SAE AS 81935 : 2011 BEARINGS, PLAIN, ROD END, SELF-ALIGNING, SELF-LUBRICATING, GENERAL SPECIFICATION FOR (-65 TO +325 DEGREES F)
    SAE AMS 4640 : 2011 ALUMINUM BRONZE, BARS, RODS, SHAPES, TUBES, AND FORGINGS, 81.5CU - 10.0AL - 4.8NI - 3.0FE, DRAWN AND STRESS RELIEVED (HR50) OR TEMPER ANNEALED (TQ50)
    MIL DTL 83488 : D COATING, ALUMINUM, HIGH PURITY
    MIL PRF 81322 : G GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395
    SAE ARP 5935 : 2013 USE OF HVOF THERMAL SPRAY COATINGS FOR HARD CHROME REPLACEMENT IN LANDING GEAR APPLICATIONS
    SAE AS 14101 : 2010 BEARING, PLAIN, SELF-LUBRICATING, SELF-ALIGNING, LOW SPEED, NARROW, GROOVED RACE, -65 TO +325 DEGREES F
    SAE AS 14104 : 2010 BEARING, PLAIN, SELF-LUBRICATING, SELF-ALIGNING, LOW SPEED, NARROW, CHAMFERED RACE, -65 TO +325 DEGREES F
    ASTM E 1444 : 2005 Standard Practice for Magnetic Particle Testing
    SAE AS 81934/2 : 2004 BEARING, SLEEVE, FLANGED, SELF-LUBRICATING, -65 TO 325 DEGREE F
    SAE AMS 4535 : 2015 COPPER-BERYLLIUM ALLOY, MECHANICAL TUBING 98CU - 1.9BE SOLUTION AND PRECIPITATION HEAT TREATED (TF00, FORMERLY AT)
    MIL PRF 16173 : E CORROSION PREVENTATIVE COMPOUND, SOLVENT CUTBACK, COLD-APPLICATION
    MIL-B-8943 Revision A:1966 BEARINGS, JOURNAL - PLAIN AND FLANGED, TFE-LINED
    SAE AS 14102 : 2010 BEARING, PLAIN, SELF-LUBRICATING, SELF-ALIGNING, LOW SPEED, WIDE, CHAMFERED RACE, -65 TO +325 DEGREES F
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