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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 1994
PAGES 19
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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 Sept. 1, 1994
Language en - English
Page Count 19
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
Sept. 1, 1994 ARP4028 Revision