SAE ARP 5794A:2018 PDF Download
Standard EN Sample
Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard
Also Known As: SAE ARP5794A, SAE ARP 5794
SAE ARP 5794A:2018 is an aerospace standard that outlines the requirements, design considerations, and testing procedures for centrifugal aircraft fuel pumps. Specifically, it focuses on fuel booster pumps that are mounted on aircraft tanks, and are responsible for feeding fuel to the engines, transferring fuel between tanks, and enabling fuel jettisoning.
The standard covers various aspects of the design and operation of these fuel pumps, with the goal of ensuring their safe and reliable performance. It sets out guidelines for pump output pressure, flow rate, and efficiency, as well as requirements for materials used in their construction and installation considerations. The standard also details the various tests and procedures that need to be conducted to validate the performance and safety of the fuel pumps, including pressure, vibration, and environmental tests.
| Descriptors | Stop / start technology; Military aircraft; Finishing; Jet fuel; Lightning protection; Failure modes and effects analysis; Magnesium alloys; Fuel pumps; Aluminum alloys; Fuel tanks |
| ICS Codes | 77.120.20 - Magnesium and magnesium alloys 91.120.40 - Lightning protection |
| Language(s) | English |
| File Size | 184.3 KB |
