SAE ARP 6166:2016-09-12

This test method is designed to simulate the synergistic combinations of oil flow, temperature cycling, hot spots, and tribology that would typically be found in a gas turbine engine. The method is intended to quantitatively characterize changes in four basic oil properties that are brought about by exposure to the afore mentioned simulated turbine engine environment: the tendency of aviation lubricants to form coke deposits, viscosity changes, total acid number changes (TAN), and oil consumption.

Author	SAE
Editor	SAE
Document type	Standard
Format	File
Confirmation date	2016-09-12
ICS	49.050 : Aerospace engines and propulsion systems 75.100 : Lubricants, industrial oils and related products
Number of pages	35
Set	AEROPAKS10U-10
Year	2016
Country	USA
Keyword	SAE 6166;SAE ARP6166;SAE ARP6166;SAE ARP 6166