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Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard
- Aerospace Standard
Published May 16, 2018 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers the general design, testing, and safety requirements for aircraft tank mounted fuel booster pumps used for engine fuel feed, transfer, and jettison.
This Aerospace Recommended Practice is intended to provide general guidelines for the design, development, and qualification of aircraft, tank mounted fuel booster pumps. This revision adds references to SAE documents ARP594 and ARP6385 which provide additional details on proper methods for thermal, mechanical, and electrical safety design of pump components.
|Aerospace Standard||Aircraft Fuel Pump Mechanical and Electrical Safety Design|
|Aerospace Standard||Sealing of Integral Fuel Tanks|
|Aerospace Standard||Composite Fuel Tanks, Fuel System Design Considerations|
Data Sets - Support Documents
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|Unnamed Dataset 2|
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|Table 1||Endurance test conditions|
|Table 2||Dielectric test voltages|
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