ARP5794A: Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard - Recommended Practice

Features

Issuing Committee: AE-5B Aircraft and Engine Fuel and Lubricant Sys Components

Scope

Content: 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.

Rationale

Content: 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.

Meta Tags

Topics: Stop / start technology
Military aircraft
Finishing
Jet fuel
Lightning protection
Failure modes and effects analysis
Magnesium alloys
Fuel pumps
Aluminum alloys
Fuel tanks

Details

DOI: https://doi.org/10.4271/ARP5794A

Pages: 1

Citation: SAE International Recommended Practice, Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard, SAE Standard ARP5794A, Revised May 2018, Issued October 2014, https://doi.org/10.4271/ARP5794A.

Additional Details

Publisher: SAE International

Published: May 16, 2018

Product Code: ARP5794A

Content Type: Recommended Practice

Status: Revised

Language: English

Historical