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 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.
SAE ARP1665A-1997 Referenced Document
SAE AS1284 STANDARD TEST PROCEDURE AND LIMIT VALUE FOR SHUTOFF SURGE PRESSURE OF PRESSURE FUEL DISPENSING SYSTEMS*， 2011-08-15 Update
SAE ARP1665A-1997 history
2007SAE ARP1665A-2007 Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft
1997SAE ARP1665A-1997 Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft
1983SAE ARP1665-1983 Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft