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SAE ARP4028

Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation
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SAE ARP4028

Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation

PUBLISH DATE 2020
PAGES 19
SAE ARP4028
This procedure is intended to apply to all engine or airframe mounted fuel pumps and controls when required by the applicable specification. The procedure recommends a recirculation system similar to ARP492 to control the fuel properties affecting the fluid and its ability to "release" fuel vapors and dissolved air and have these "re-entrained or dissolved" during the fluid recovery process back to the tank and the original starting conditions.
SDO SAE: SAE International
Document Number ARP4028
Publication Date April 29, 2020
Language en - English
Page Count 19
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
April 29, 2020 ARP4028 Revision