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Aircraft/Engine Fuel Pump Net Positive Suction Pressure Performance Test and Evaluation
- Aerospace Standard
Published April 29, 2020 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This procedure applies to engine or airframe-mounted fuel pumps. The procedure recommends single-pass operation to minimize changes in fuel properties affecting NPSP capability. An optional method using a recirculation system is also included and may be specified at the discretion of the equipment specification.
This procedure defines the recommended test setup, test procedure, data acquisition, and data presentation.
ARP4024 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||Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems|
|Aerospace Standard||Aircraft Engine Fuel Pump Cavitation Endurance Test|
Data Sets - Support Documents
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|AIR1326||AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER|
|ARP492||Aircraft Engine Fuel Pump Cavitation Endurance Test|
|ASTMD1298||This document is not part of the subscrption.|
|ASTMD270||This document is not part of the subscrption.|
|ASTMD323||This document is not part of the subscrption.|
|ASTMD3827||This document is not part of the subscrption.|
|ASTMD4057||This document is not part of the subscrption.|
|MIL-G-5572||This document is not part of the subscrption.|
|MIL-T-5624||This document is not part of the subscrption.|
|MIL-T-83133||This document is not part of the subscrption.|
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