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Aircraft Design Engineering and Styling AE-5B Aircraft and Engine Fuel and Lubricant Sys Components Failure modes and effects analysis (FMEA)

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Aircraft Fuel Pump Mechanical and Electrical Safety Design
2022-10-18
CURRENT
ARP6385
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.
Standard

Impact of Copper Contamination on the Thermal Stability of Jet Fuels
2019-04-11
CURRENT
AIR6443
This SAE Aerospace Information Report (AIR) discusses the sources of Copper in aviation jet fuels, the impact of Copper on thermal stability of jet fuels and the resultant impact on turbine engine performance, and potential methods for measurement and reduction of the catalytic activity of Copper contamination in jet fuels. This document is an information report and does not provide recommendations or stipulate limits for Copper concentrations in jet fuels.
Standard

Fuel Pump Thermal Safety Design
2022-10-18
CURRENT
ARP594F
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.
Standard

Fuel Pump Thermal Safety Design
2016-05-24
HISTORICAL
ARP594E
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.
Standard

AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER
1974-01-01
HISTORICAL
AIR1326
The AIR is limited to a presentation of the historical background, the technical rationale which generated the V/L fuel condition interface requirement in specifications between the aircraft fuel delivery system and the aircraft engine fuel system, and limitations in the usage of the V/L concept.
Standard

Aircraft Fuel System Vapor-Liquid Ratio Parameter
2020-04-29
CURRENT
AIR1326A
The AIR is limited to a presentation of the historical background, the technical rationale which generated the V/L fuel condition interface requirement in specifications between the aircraft fuel delivery system and the aircraft engine fuel system, and limitations in the usage of the V/L concept.
Standard

GEARBOX - AIRFRAME MOUNTED ACCESSORY
1991-06-01
HISTORICAL
ARP1961
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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