AS83819 Bearings, Plain, Self-Aligning, Self-Lubricating, 1400 cpm (15 fpm), Oscillation, -65 to +160 °F (-54 to +71 °C)

Current

08/23/2018

Features
Issuing Committee
Scope
Content
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 1400 cpm (15 fpm). 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.
Rationale
Content
The reason for creating this standard is to qualify bearings for tail rotor bearing applications. The standard also incorporates an ‘A’ part number designation for a new liner system that has 2-1/2 times the life of the standard liner system.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS83819
Pages
26
Citation
SAE International Technical Standard, Bearings, Plain, Self-Aligning, Self-Lubricating, 1400 cpm (15 fpm), Oscillation, -65 to +160 °F (-54 to +71 °C), SAE Standard AS83819, Reaffirmed August 2018, Issued May 2013, https://doi.org/10.4271/AS83819.
Additional Details
Publisher
Published
Aug 23, 2018
Product Code
AS83819
Content Type
Technical Standard
Status
Current
Language
English

Revisions