Aircraft and Aircraft Engine Fuel Pump Low Lubricity Fluid Endurance Test
Performance Evaluation of Fuel Filter Elements Utilized in Aircraft Gas Turbine Engine/APU Main Fuel Systems
Measuring Aircraft Gas Turbine Engine Fine Fuel Filter Element Performance
Lubrication System Oil Tank Sizing
Fuel Pump Thermal Safety Design
Aircraft Fuel Pump Mechanical and Electrical Safety Design
Transmitter, Pressure, Fuel, 0-600 psi
Considerations for Ground Fault Interrupter (GFI) / Arc Fault Circuit Breaker (AFCB) for fuel pumps power circuit protection installation, specification and testing
Aircraft Engine Fuel Pump Cavitation Endurance Test
If any of the above conditions do not apply, refer to Section 2.
The procedure recommended herein is based on experience gathered by a number of laboratories conducting component qualification tests to MIL-E-5009, currently MIL-E-5007. It is intended to produce a uniform reproducible steady state test condition for fuel pump cavitation testing as required by various military engine specifications.
This test is not intended to establish altitude or climb rate, starting, or other transient performance of the article tested.