SAE AS82819
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Bearings, Plain, Self-Aligning, Self-Lubricating, 300 cpm Oscillation (13 fpm), -65 to +160 °F (-54 to +71 °C), Liners Less Than 0.015 inches
25-09-2020
23-08-2018
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Specifies the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 degrees F (-54 to +71 degrees C) at high cyclic speeds 300 cpm (13 fpm) for liners with a thickness less than 0.015 inch.
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 °F (-54 to +71 °C) at high cyclic speeds 300 cpm (13 fpm) for liners with a thickness less than 0.015 inch. The scope of this standard is to provide a liner system qualification procedure for helicopter sliding bearings defined and controlled by source control drawings. Once a liner system is qualified, the source-controlled bearings are further tested under application conditions.Under Department of Defense (DoD) Policies and Procedures, any qualification requirements and associated Qualified Products List (QPLs) are mandatory for DoD contracts. Any materials relating to QPLs have not been adopted by SAE and are not part of this SAE technical document.
| MIL-DTL-197 Revision M:2016 | PACKAGING OF BEARINGS, ASSOCIATED PARTS AND SUBASSEMBLIES |
| SAE ARP5448/7A | Plain Bearing Wear Measurement |
| SAE AMS1424M | Deicing/Anti-Icing Fluid, Aircraft SAE Type 1 |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| SAE AMSQQP416E | Plating, Cadmium (Electrodeposited) |
| 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) |
| SAE AMS2417J | Plating, Zinc-Nickel Alloy |
| SAE ARP 5448/2 : 2007 | PLAIN BEARING HIGH SPEED OSCILLATION TEST |
| 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 |
| SAE AS82819/1 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, 300 CPM (13 FPM) OSCILLATION, -65 TO +160 °F, LINERS LESS THAN .015 INCH THICK |
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