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Research and development Product development G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies Thermodynamics Design Engineering and Styling Sensors and actuators

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Standard

Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
2006-08-31
HISTORICAL
AS1710C
This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits.
Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
2005-06-02
HISTORICAL
AS1650A
This aerospace specification defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure.
Standard

Test Methods, Hose Assemblies, Polytetrafluoroethylene (PTFE), Metric
2004-07-08
HISTORICAL
MA2078A
This SAE Aerospace Standard describes the test methods for flexible PTFE hose and hose assemblies used in aircraft fluid systems in the pressure and temperature ranges defined in MA2001 (ISO 6771). It applies to the hose and the hose coupling. The tests and assembly requirements for the connecting end fitting are covered in the procurement specification. This document applies each time that it is referred to in a procurement specification or other definition document. Fluids and materials used for the tests are listed in Appendix A.
Standard

Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
2004-05-03
HISTORICAL
AS1710B
This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to 200 °F and at 125 psi peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits.
Standard

V-Couplings, Application of
2004-04-27
HISTORICAL
AIR869A
This SAE Aerospace Information Report is intended to inform users of the proper use, application, and installation of V-couplings. V-couplings will perform only if they are properly installed. This document informs the user of the correct manner of applying and installing V-couplings and also cautions against improper use.
Standard

COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING
1998-03-01
HISTORICAL
AS1650
This document defines the requirements for a threadless, flexible, self-bonding coupling assembly, which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent, or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -65 to 400 °F and at 125 psi operating pressure.
Standard

TEST METHODS, HOSE ASSEMBLIES, TETRAFLUOROETHYENE (TFE)
1986-01-01
HISTORICAL
MA2078
This standard describes the test methods for flexible TFE hose and hose assemblies used in aircraft fluid systems in the pressure and temperature ranges covered by pressure classes B, D and E, and temperature types I, II and III of MA 2001 - ISO 6771. It applies to the hose and the hose coupling. The tests and assembly requirements for the connecting end fitting are covered in the procurement specification. This standard applies each time that it is referred to in a procurement specification or other definition document. Fluids and materials used for the tests are listed in Appendix A.
Standard

COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY, THREADED TYPE WITH FERRULES
1984-01-01
HISTORICAL
AS1710A
This specification defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel, vent or other systems. This coupling assembly is designed for use from -65 to 200 degrees F and at 125 psi peak working pressure.
Standard

COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY THREADED TYPE WITH FERRULES
1982-05-01
HISTORICAL
AS1710
This specification defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings, to join tubing and components in aircraft fuel, vent or other systems. This coupling assembly is designed for use from -65 to 200 degrees F and at 125 psi operating pressure.
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