SAE AS81934B
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Bearings, Sleeve, Plain and Flanged, Self-Lubricating
Hardcopy , PDF
08-11-2019
English
06-05-2016
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1. SCOPE
2. REFERENCES
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Specifies plain and flanged sleeve bearings which are self-lubricating by incorporating polytetrafluoroethylene (PTFE) in a liner in the bore for use in the temperature range of -65 to +325 degrees F.
| DevelopmentNote |
Supersedes MIL B 81934. (04/2001)
|
| DocumentType |
Standard
|
| Pages |
19
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This standard covers plain and flanged sleeve bearings which are self-lubricating by incorporating polytetrafluoroethylene (PTFE) in a liner in the bore for use in the temperature range of -65 to +325 °F.
| MIL-DTL-24151 Revision B:2016 | DOORS, ROLLER CURTAIN AND HINGED SLAT, AND ASSOCIATED OPERATING EQUIPMENT |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| MIL-DTL-197 Revision M:2016 | PACKAGING OF BEARINGS, ASSOCIATED PARTS AND SUBASSEMBLIES |
| MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
| SAE AIR5883 | Landing Gear Shock Struts Bearing Selection |
| SAE ARP5448/9A | Plain Bearing Lined Inside Diameter Plug Gaging |
| SAE AIR1594C | Plain Bearing Selection for Landing Gear Applications |
| SAE AS81934/1A | BEARING, SLEEVE, PLAIN, SELF-LUBRICATING, −65 °F TO 325 °F |
| MIL-DTL-197 Revision M:2016 | PACKAGING OF BEARINGS, ASSOCIATED PARTS AND SUBASSEMBLIES |
| SAE AMS1424M | Deicing/Anti-Icing Fluid, Aircraft SAE Type 1 |
| SAE AS8243 | Anti-Icing and Deicing-Defrosting Fluids |
| SAE AMSQQP416E | Plating, Cadmium (Electrodeposited) |
| SAE AS81820D | Bearings, Plain, Self-Aligning, Self-Lubricating, Low Speed Oscillation |
| MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
| MIL-PRF-7808 Revision L:1997 | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MIL-DTL-5541 Revision F:2006 | Chemical Conversion Coatings on Aluminum and Aluminum Alloys |
| SAE AMS2417J | Plating, Zinc-Nickel Alloy |
| SAE AS14101D | BEARING, PLAIN, SELF-LUBRICATING, SELF-ALIGNING, LOW SPEED, NARROW, GROOVED RACE, -65 TO +325 °F |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-DTL-83133 Revision J:2015 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
| SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
| SAE AS81934/2A | BEARING, SLEEVE, FLANGED, SELF-LUBRICATING, −65 °F TO 325 °F |
| SAE AMS2700E | Passivation of Corrosion Resistant Steels |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| MIL-HDBK-1599 Revision A:1997 | BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS |
| SAE ARP5448/9A | Plain Bearing Lined Inside Diameter Plug Gaging |
| ASME Y14.100 : 2017 | ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| ASTM F 25 : 2004 | Standard Test Method for Sizing and Counting Airborne Particulate Contamination in Cleanrooms and Other Dust-Controlled Areas |
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