This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Aircraft Engine Fuel Pump Cavitation Endurance Test
- Aerospace Standard
Published July 18, 2014 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft engine fuel pumps for the purpose of determining their resistance to deterioration, during steady state endurance test, while receiving MIL-T-5624 Grade JP-4 fuel as a homogenous mixture of gas and liquid expressed as a ratio of vapor volume to liquid volume (V/L).
If any of the above conditions do not apply, refer to Section 2.
ARP492C has been reaffirmed to comply with the SAE five-year review policy.
|Aerospace Standard||Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation|
|Aerospace Standard||Fuel Pump Thermal Safety Design|
|Aerospace Standard||Aircraft Fuel System Vapor-Liquid Ratio Parameter|
Data Sets - Support Documents
|[Unnamed Dataset 1]|
|TABLE A1||Corrections to Absolute True Vapor Pressure for Distallation Slope|
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.