This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Aircraft and Aircraft Engine Fuel Pump Low Lubricity Fluid Endurance Test
- Aerospace Standard
Published December 11, 2014 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This procedure is intended to apply to fuel pumps.
This procedure will be defined in terms of recommended test fluid, test setup, test conditions, and test method.
This procedure may be used for other fuel system components, by testing in conjunction with the pump, which normally supplies the component inlet flow, or a substitute test pump of similar capacity.
This procedure may be used, with variations in test conditions and test fluid for performing pump evaluation tests. Tests at progressively increasing pump speeds and pressures will provide design limitation data. Alternate test periods on a test pump and another pump, of a design for which actual service durability is known, will provide useful comparison data.
ARP1797A has been reaffirmed to comply with the SAE five-year review policy.
|Aerospace Standard||Performance Testing of Lubricant Filter Elements Utilized in Aircraft Power and Propulsion Lubrication Systems|
|Aerospace Standard||Detailed Specification for Aircraft Pressure Refueling Nozzle|
|Aerospace Standard||Life Rafts|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
* 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.