SAE ARP 1665 : 2007

Table of Contents

1 SCOPE
2 REFERENCES
3 CRITICAL PARAMETERS
4 SURGE PRESSURE DEFINITION
5 INSTRUMENTATION
6 PRETEST CALIBRATION
7 TEST PROCEDURE
8 SYSTEM SIMULATION

Abstract

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.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	AE-5