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Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft
- Aerospace Standard
- ARP1665A
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Scope
The test procedure applies to the refueling manifold system connecting the receiver aircraft fuel tanks to the refueling source fuel pump(s) for both ground and aerial refueling. The test procedure is intended to verify that the limit value for surge pressure specified for the receiver fuel system is not exceeded when refueling from a refueling source which meets the requirements of AS1284 (reference 2). This recommended practice is not directly applicable to surge pressure developed during operation of an aircraft fuel system, such as initiating or stopping engine fuel feed or fuel transfer within an aircraft, or the pressure surge produced when the fuel pumps are first started to fill an empty fuel manifold.
Recommended Content
Aerospace Standard | Standard Test Procedure and Limit Value for Shutoff Surge Pressure of Pressure Fuel Dispensing Systems |
Aerospace Standard | Thesaurus for Fuel System Components |
Technical Paper | Pressure Transients in Aerial Refueling Systems |
Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee
Welcome to the AE-5A, 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 |
---|---|
AS1284 | STANDARD TEST PROCEDURE AND LIMIT VALUE FOR SHUTOFF SURGE PRESSURE OF PRESSURE FUEL DISPENSING SYSTEMS |
ENFEF-TM-81-03 | This document is not part of the subscrption. |
HYTRAN Report MDCA3060 | This document is not part of the subscrption. |
HYTRANReportMDC | This document is not part of the subscrption. |
MIL-F-17874B | This document is not part of the subscrption. |
MIL-F-87154 | This document is not part of the subscrption. |
MIL-T-83219 | This document is not part of the subscrption. |
NAVAIR06-5-504 | This document is not part of the subscrption. |
RPL-TDR-64-25 | This document is not part of the subscrption. |
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