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SAE ARP6385

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Aircraft Fuel Pump Mechanical and Electrical Safety Design

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The requirements presented in this document address the key considerations for mechanical and electrical safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.

SDO SAE: SAE International
Document Number ARP6385
Publication Date Oct. 10, 2017
Language en - English
Page Count 12
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
Oct. 10, 2017 ARP6385 Revision