SAE ARP4028 PDF
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Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation
Description
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.
History
| ARP4028 | 2020-04-29 | Latest | Reaffirmed |
| ISSUING COMMITTEE | AE-5B Aircraft and Engine Fuel and Lubricant Sys Components |
|---|---|
| DATE | 2020-04-29 |
| DOI | |
| ISCURRENT | Current |
| PAGE | 19 |
| PUBLISHER | SAE International |
| REVISED | REAFFIRMED |
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