Browse Standards ARP6917
Current ISSUED 2018-12-10

Evaluation of Gas Turbine Engine Lubricant Compatibility with Elastomer Slabs - Long Duration Test ARP6917

This test method provides procedures for exposing specimens of elastomer material (slab form) representative to those used in gas turbine engines to aviation lubricants under extended duration and engine relevant thermal conditions. For AS5780 requirements the time is at least 1800 hours and temperatures are 100 °C to 160 °C. Positive volume change is an indication of specimen swell and subsequent negative volume change is an indication of specimen deterioration, both properties are important in the evaluation of the compatibility of the lubricant with elastomers used in the construction of the gas turbine.
ARP6917
2018-12-10
Latest
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 10% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.
We also recommend:
STANDARD

Aviation Lubricant Tribology Evaluator (ALTE) Method to Determine the Lubricating Capability of Gas Turbine Lubricants

ARP6255

View Details

TECHNICAL PAPER

Advanced Synthetic Passenger Vehicle Engine Oils for Extended Oil Drain Performance

981444

View Details

TECHNICAL PAPER

AIRCRAFT TURBINE ENGINE SYNTHETIC LUBRICANTS AND THEIR LUBRICATING PROPERTIES

530013

View Details

Get Involved

Want to participate in updating this standard?

X