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

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • ARP5794A
  • Current
Published 2018-05-16 by SAE International in United States
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.
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Fuel Pump Thermal Safety Design

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • ARP594F
  • Current
Published 2017-11-09 by SAE International in United States
The requirements presented in this document address the key considerations for thermal safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.
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Aircraft Fuel Pump Mechanical and Electrical Safety Design

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • ARP6385
  • Current
Published 2017-10-10 by SAE International in United States
The requirements presented in this document address the key considerations for mechanical and electrical safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.
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Contaminants for Aircraft Turbine Engine Fuel System Component Testing

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • AIR4246D
  • Current
Published 2017-09-27 by SAE International in United States
This SAE Aerospace Information Report (AIR) is intended as a guide toward standardization of descriptions and specifications of fluid contamination products.
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Transmitter, Pressure, Fuel, 0-600 psi

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • AS6302A
  • Current
Published 2016-10-27 by SAE International in United States
This specification covers one type of fuel pressure transmitter designated MS28005-7.
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Ball-On-Cylinder (BOC) Aircraft Turbine Fuel Lubricity Tester

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • AIR1794B
  • Current
Published 2016-07-26 by SAE International in United States
This metric SAE Aerospace Information Report (AIR) details a ball-on-cylinder (BOC) test device and specifies a method of rating the relative lubricity of aviation turbine fuel samples. The BOC produces a wear scar on a stationary steel ball by forcing it with a fixed load against a fuel wetted steel test ring in a controlled atmosphere. The test ring is rotated at a fixed speed so its surface is wetted by a momentary exposure to the fluid under test. The size of the wear scar is a measure of the test fluid lubricity and provides a basis for predicting friction or wear problems.
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Fuel Pump Thermal Safety Design

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • ARP594E
  • Historical
Published 2016-05-24 by SAE International in United States
The requirements presented in this document cover the design factors which might cause any part of an electrically motor driven fuel pump assembly to act as an ignition source for explosive fuel vapors within the airplane tank.
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Ball-On-Cylinder (BOC) Aircraft Turbine Fuel Lubricity Tester

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • AIR1794A
  • Historical
Published 2016-05-13 by SAE International in United States
This metric SAE Aerospace Information Report (AIR) details a ball-on-cylinder (BOC) test device and specifies a method of rating the relative lubricity of aviation turbine fuel samples. The BOC produces a wear scar on a stationary steel ball by forcing it with a fixed load against a fuel wetted steel test ring in a controlled atmosphere. The test ring is rotated at a fixed speed so its surface is wetted by a momentary exposure to the fluid under test. The size of the wear scar is a measure of the test fluid lubricity and provides a basis for predicting friction or wear problems.
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Gearbox - Airframe Mounted Accessory

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • ARP1961A
  • Current
Published 2016-05-10 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) addresses the characteristics required for the definition, development, and acquisition of a satisfactory airframe mounted accessory gearbox (AMAG).
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Aircraft Turbine Fuel Contamination History and Endurance Test Requirements

AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
  • Aerospace Standard
  • AIR4023C
  • Current
Published 2016-04-10 by SAE International in United States
This document discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.
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