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Aircraft/Engine Fuel Pump Net Positive Suction Pressure Performance Test and Evaluation
- Aerospace Standard
- ARP4024
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
ARP4024 has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
Aerospace Standard | Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation |
Aerospace Standard | Aircraft Engine Fuel Pump Cavitation Endurance Test |
Aerospace Standard | Contaminants for Aircraft Turbine Engine Fuel System Component Testing |
Data Sets - Support Documents
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Issuing Committee
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Welcome to the AE-5B, Aerospace Fuel, Inerting and Lubriation Systems public forum area.
Scope: Has responsibility for the resolution of problems in either design or service usage of aerospace fuel, oil and oxidizer systems, their components such as valves, pumps, couplings, fuel cells, quantity and flow gages, and tanks, and related problems as presure surger, icing, electrification, and safety. Develops standards addressing fuel, oil and oxidizer systems. For details about SAE's online privacy policy; copyright, content license, and reliability statements; and membership information, click on the link to "Info on Privacy, Copyright, and Membership" link in the folders area below. No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.Reference
Number | Title |
---|---|
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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