SAE AS83819

Detailinformationen

Bezeichnung: SAE AS83819

Ausgabedatum: 01.08.2018

Seiten: 0

Land: Amerikanische technische Norm

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Annotation

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.

SUBJECT TAXONOMY: Aircraft structures, Airframes, Fuselages, Materials, Bearings, Tests and Testing
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard