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Standard

Synthetic Jet Fuels from Non-Petroleum Feed Stocks
2023-02-20
CURRENT
AIR6148
This SAE Aerospace Information Report (AIR) provides general information on the developing subject of synthetic jet fuels derived from non-petroleum feed stocks. It addresses synthetic jet fuel properties and other topics associated with their use and is intended as a guide to assist aviation fuel system designers in considering important information on fuel properties when designing aircraft fuel systems and components. The AIR is limited to “drop-in” fuels that meet the requirements of the respective fuel specifications and are compatible with typical aircraft and ground refueling systems. While some key properties are included in this AIR for discussion, the reader should utilize documents such as MIL-HDBK-510 or the ASTM International research reports for a more-detailed review of fuel properties. AIR7484 also gives more details on fuel properties, specifically as they relate to airframe fuel system design.
Standard

Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems
2020-03-19
CURRENT
AIR1616B
MIL-STD-1290, 14 CFR 27.952, and 14 CFR 29.952 provide crash resistant fuel system design and test criteria that significantly minimize fuel leaks and occurrence of post-crash fire in survivable impacts. This document does not change and does not authorize changes in or deviations from MIL-Standard or regulatory requirements. This document provides guidance for the design, performance, and test criteria for self-sealing breakaway valves.
Standard

Recommendations for Fuel and Oil System Schematics
2019-05-07
CURRENT
ARP1482B
This document recommends and sets forth a set of symbols representing the components making up aircraft fuel and oil systems. The intended result is uniformity in system schematics so that they may be easily understood throughout the aerospace industry.
Standard

Nozzles and Ports – Gravity Fueling Interface Standards for Civil Aircraft
2012-01-03
CURRENT
AS1852D
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

Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft
1997-08-01
HISTORICAL
AS1852B
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. In addition, this document defines the minimum fuel nozzle tip dimensions for turbine fuel ground service equipment and the maximum fuel nozzle tip diameter for gasoline ground service equipment.
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
2013-08-09
HISTORICAL
ARP868C
This document provides recommended methods and describes associated equipment and test setups to assist in understanding and conducting pressure drop tests on fuel system components. Background information and suggestions are provided as means of improving accuracy and repeatability of test results. Although written specifically for fuel system components, the methods, equipment and suggestions presented herein apply equally to pressure drop tests of other liquid-handling devices.
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.
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