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Conductivity Joining Metallurgy Standardization Metals AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee

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Standard

Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft
2006-03-24
HISTORICAL
AS1852C
This SAE Aerospace Standard (AS) defines the maximum allowable free opening dimensions for airframe fueling ports on civil aircraft that require the exclusive use of gasoline as an engine fuel, and the minimum free opening dimensions for airframe fueling ports on civil aircraft that operate with turbine fuels as the primary fuel type and with gasoline as the emergency fuel type. This SAE Aerospace Standard (AS) also defines the features and dimensions for airframe refueling ports on civil aircraft that require the exclusive use of turbine fuel as an engine fuel. In addition, this document defines the minimum fuel nozzle spout dimensions for turbine fuel ground service equipment, and the maximum fuel nozzle spout diameter for gasoline ground service equipment.
Standard

Minimization of Electrostatic Hazards in Aircraft Fuel Systems
2013-08-09
HISTORICAL
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
1994-09-01
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

GLOSSARY OF TERMS - AIRCRAFT GROUND REFUELING
2007-12-04
HISTORICAL
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
2022-10-04
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
2007-12-04
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

Aircraft Flexible Tanks General Design and Installation Recommendations
2019-05-07
CURRENT
AIR1664A
This SAE Aerospace Information Report (AIR) includes general information about the various types and styles of flexible tanks and the tank-mounted fittings that adapt the tank to the surrounding structure and fluid-system plumbing. Recommendations are given relative to the dimensional layout of the tank when these recommendations serve to avoid tank fabrication problems and tank/structure interface problems. As a part of these recommendations, critical dimensions of plumbing adapter fittings are discussed and recommendations made. Tank manufacturing tolerances are given. Recommendations are made relative to cavity design and preparation to facilitate a reliable installation. The special installation requirements of nonself-sealing, self-sealing, and crash-resistant tanks are discussed. This document is not intended to replace the information or requirements of the military and commercial procurement specifications listed in Section 2.
Standard

AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS
1994-09-01
HISTORICAL
AIR1664
This Aerospace Information Report (AIR) includes general information about the various types and styles of flexible tanks and the tank-mounted fittings that adapt the tank to the surrounding structure and fluid-system plumbing. Recommendations are given relative to the dimensional layout of the tank when these recommendations serve to avoid tank fabrication problems and tank/structure interface problems. As a part of these recommendations, critical dimensions of plumbing adapter fittings are discussed and recommendations made. Tank manufacturing tolerances are given. Recommendations are made relative to cavity design and preparation to facilitate a reliable installation. The special installation requirements of non-self-sealing, self-sealing, and crash-resistant tanks are discussed. This document is not intended to replace the information or requirements of the military and commercial procurement specifications listed in section 3.
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