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Hydraulic fluids Joining Parts Identification Metals Metallurgy AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee

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Standard

ACCEPTANCE TEST PROCEDURES AND STANDARDS TO INSURE CLEAN FUEL SYSTEM COMPONENTS
2007-12-04
HISTORICAL
ARP1953A
To describe general guidelines for achieving selected levels of cleanliness in gas turbine engine fuel system components and to describe laboratory type methods for measuring and reporting the contamination level of the wetted portion of fuel system components. As in SAE J1227 (covering hydraulic components) this practice includes guidelines for levels of acceptance but does not attempt to set those levels.
Standard

ACCEPTANCE TEST PROCEDURES AND STANDARDS TO INSURE CLEAN FUEL SYSTEM COMPONENTS
1992-08-01
HISTORICAL
ARP1953
To describe general guidelines for achieving selected levels of cleanliness in gas turbine engine fuel system components and to describe laboratory type methods for measuring and reporting the contamination level of the wetted portion of fuel system components. As in SAE J1227 (covering hydraulic components) this practice includes guidelines for levels of acceptance but does not attempt to set those levels.
Standard

Acceptance Test Procedures and Standards to Ensure Clean Fuel System Components
2020-10-01
CURRENT
ARP1953B
To describe general guidelines for achieving selected levels of cleanliness in gas turbine engine fuel system components and to describe laboratory methods for measuring and reporting the contamination level of the wetted portion of fuel system components. As in SAE J1227 (covering hydraulic components) this practice includes guidelines for levels of acceptance but does not attempt to set those levels.
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

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.
Standard

Impact of Changes in Test Dust Contaminants and Particle Counter Calibration on Laboratory Filter Element Performance and Fluid Cleanliness Classes
2003-07-03
HISTORICAL
AIR5455
This SAE Aerospace Information Report (AIR) discusses the impact of the ISO Test Dusts, chosen as replacement contaminants for the Arizona Test Dusts (AC Test Dusts), and the ISO calibration procedure ISO 11171 for automatic particle counters, which replaces the calibration procedure ISO 4402 (1991), on laboratory performance of filter elements utilized in aerospace lubrication, hydraulic and fuel systems, and fluid cleanliness levels determined with automatic particle counters.
Standard

Impact of Changes in Test Dust Contaminants and Particle Counter Calibration on Laboratory Filter Element Performance and Fluid Cleanliness Classes
2012-01-03
CURRENT
AIR5455A
This SAE Aerospace Information Report (AIR) discusses the impact of the ISO Test Dusts, chosen as replacement contaminants for the Arizona Test Dusts (AC Test Dusts), and the ISO calibration procedure ISO 11171 for automatic particle counters, which replaces the calibration procedure ISO 4402 (1991), on laboratory performance of filter elements utilized in aerospace lubrication, hydraulic and fuel systems, and fluid cleanliness levels determined with automatic particle counters.
Standard

Thesaurus for Fuel System Components
2007-12-04
HISTORICAL
AIR1615A
This document provides a summary of names commonly used throughout the industry for aircraft fuel system components. It is a thesaurus intended to aid those not familiar with the lexicon of the industry.
Standard

Thesaurus for Fuel System Components
2020-02-24
CURRENT
AIR1615B
This document provides a summary of names commonly used throughout the industry for aircraft fuel system components. It is a thesaurus intended to aid those not familiar with the lexicon of the industry.
Standard

GRAVITY REFUELING NOZZLES AND PORTS INTERFACE STANDARD FOR CIVIL AIRCRAFT
1984-12-01
HISTORICAL
AS1852
This Aerospace Standard (AS) defines maximum free opening dimensions for airframe refueling ports on civil aircraft that require the exclusive use of aviation gasolines, and minimum free opening dimensions for airframe refueling ports on civil aircraft that operate with turbine fuels as a primary fuel type. In addition, this document defines the minimum refueling nozzle tip dimensions for turbine fuels ground service equipment, and the maximum refueling nozzle tip diameter dimension for aviation gasolines ground service equipment.
Standard

GRAVITY REFUELING NOZZLES AND PORTS INTERFACE STANDARD FOR CIVIL AIRCRAFT
1988-02-01
HISTORICAL
AS1852A
This AS defines maximum free opening dimensions for airframe refueling ports on civil aircraft that require the exclusive use of aviation gasolines, and minimum free opening dimensions for airframe refueling ports on civil aircraft that operate with turbine fuels as a primary fuel type. In addition, this document defines the minimum refueling nozzle tip dimensions for turbine fuels ground service equipment, and the maximum refueling nozzle tip diameter dimension for aviation gasolines ground service equipment.
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