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SAE ARP5794

Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard

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Organization: SAE
Publication Date: 1 May 2018
Status: active
Page Count: 25
scope:

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.

Purpose

This document is intended to provide guidance for the proper design, testing, and certification of aircraft, tank mounted fuel pumps. References to key considerations for safety compliance to all applicable industry regulations are directly discussed or references are provided to other SAE documents. This document is meant to complement a Procurement Agency's detail technical specification for a given design application or use. This document was developed as the replacement document for MIL-P-5238C, which was made inactive in 1996.

intended Use:

The pumps covered by this specification are intended for use in aircraft fuel tanks to pump fuel to the engines or to transfer fuel from tank to tank. Refer to the product's detail specification... View More

Document History

SAE ARP5794
May 1, 2018
Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard
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. Purpose This document...
October 1, 2014
Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard
This specification covers the general requirements for aircraft tank mounted, centrifugal type, fuel booster pumps, used for engine fuel feed and/or fuel transfer. Purpose This document is intended...

References

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