SAE International Aircraft Fuel Pump Mechanical and Electrical Safety Design ARP6385

Description
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.
Description
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.

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Aircraft Fuel Pump Mechanical and Electrical Safety Design - ARP6385 - SAE International
Warrendale, PA, United States
Aircraft Fuel Pump Mechanical and Electrical Safety Design
ARP6385
Aircraft Fuel Pump Mechanical and Electrical Safety Design ARP6385
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.

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.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number ARP6385
Product Name Aircraft Fuel Pump Mechanical and Electrical Safety Design
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