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Standard

Minimization of Electrostatic Hazards in Aircraft Fuel Systems

1998-09-01
CURRENT
AIR1662A
This SAE Aerospace Information Report (AIR) provides background information, technical data and related technical references for minimization of electrostatic hazards in aircraft fuel systems. Techniques used to minimize the electrostatic hazard include: a Reducing fueling rate into tank bays including use of multiple refueling inlet nozzles. b Reducing refuel plumbing flow velocities. c Introducing fuel into the tank at a low velocity near the bottom and directing it to impinge upon a grounded conducting surface. d Avoiding electrically isolated conductors in the fuel tank. e Using conductivity additives in the fuel.
Standard

METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS

1990-12-18
HISTORICAL
ARP868B
To describe useful methods for conducting pressure drop tests of fuel system components for MIL-F-8615 or similar requirements and to present general suggestions for improving accuracy of test results.
Standard

METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS

1983-06-01
HISTORICAL
ARP868A
To describe useful methods for conducting pressure drop tests of fuel system components for MIL-F-8615 or similar requirements; and to present general suggestions for improving accuracy of test results.
Standard

Guidance on the Impact of Fuel Properties on Fuel System Design and Operation

2018-02-24
CURRENT
AIR7484
This document describes a number of jet fuel properties and where applicable gives the specification limits for Jet A and Jet A-1, though the properties are generally applicable to all turbine fuels. Later versions of this document will give more details on specification limits for other similar fuels, such as TS-1, where they differ from Jet A and Jet-A1. It gives details about the possible impact on airframe fuel system design.
Standard

GLOSSARY OF TERMS - AIRCRAFT GROUND REFUELING

1994-03-01
CURRENT
AIR4783
This SAE Aerospace Information Report (AIR) presents a glossary of terns commonly utilized in the ground delivery of fuel to an aircraft and some terms relating to the aircraft being refueled.
Standard

FLUID SYSTEM COMPONENT SPECIFICATION PREPARATION CRITERIA

1983-06-01
HISTORICAL
AIR1082A
The "Scope" section may be a very brief statement describing the coverage of the specification for a simple device, or it may require a long description of limiting parameters for a more complex device or system having a complicated interface definition.
Standard

Electrical Bonding of Aircraft Fuel Systems

2012-12-18
CURRENT
AIR5128A
This SAE Aerospace Information Report (AIR) is limited to the subject of aircraft fuel systems and the questions concerning the requirements for electrical bonding of the various components of the system as related to Static Electric Charges, Fault Current, Electromagnetic Interference (EMI) and Lightning Strikes (Direct and Indirect Effects). This AIR contains engineering guidelines for the design, installation, testing (measurement) and inspection of electrical bonds.
Standard

ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEM PLUMBING SYSTEMS

1997-01-01
HISTORICAL
AIR5128
This SAE Aerospace Information Report (AIR) is limited to the subject of aircraft fuel system plumbing systems and the questions concerning the requirements for electrical bonding of the various components of the system as related to Static Electric Charges, Electromagnectic Interference (EMI) and Lightning Strikes (Direct and Indirect Effects)
Standard

Composite Fuel Tanks, Fuel System Design Considerations

2012-12-11
CURRENT
AIR5774
This SAE Aerospace Information Report (AIR) is a compilation of engineering references and data useful to the technical community that can be used to ensure fuel system compatibility with composite structure. This AIR is not a complete detailed design guide and is not intended to satisfy all potential fuel system applications. Extensive research, design, and development are required for each individual application.
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