AS5780A Specification for Aero and Aero-Derived Gas Turbine Engine Lubricants

Revised

10/14/2005

Features
Issuing Committee
Scope
Content
This specification defines basic physical, chemical, and performance limits for 5 cSt grades of gas turbine engine lubricating oils used in aero and aero-derived marine and industrial applications, along with standard test methods and requirements for laboratories performing them. It also defines the quality control requirements to assure batch conformance and materials traceability, and the procedures to manage and communicate changes in oil formulation and brand. This specification invokes the Performance Review Institute (PRI) product qualification process. Requests for submittal information may be made to the PRI at the address in Appendix C, referencing this specification. Products qualified to this specification are listed on a Qualified Products List (QPL) managed by the PRI. Additional tests and evaluations may be required by individual equipment builders before an oil is approved for use in their equipment. Approval and/or certification for use of a specific gas turbine oil in aero and aero-derived marine and industrial applications is the responsibility of the individual equipment builders and/or governmental authorities and is not implied by compliance with or qualification to this specification.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS5780A
Pages
21
Citation
SAE International Technical Standard, Specification for Aero and Aero-Derived Gas Turbine Engine Lubricants, SAE Standard AS5780A, Revised October 2005, Issued September 2000, https://doi.org/10.4271/AS5780A.
Additional Details
Publisher
Published
Oct 14, 2005
Product Code
AS5780A
Content Type
Technical Standard
Status
Revised
Language
English

Revisions