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Standard

Coupling Assembly, Hydraulic Self Sealing, Quick Disconnect

2019-02-07
WIP
AS1709B
Paragraph 2.2 add AS1241, 3.3 & 3.4.3 add AS1241 Type V, 3.4.1 add Type IV temperature limitation +250 F, 3.6.8 add Figure 1 test setup, Table V Class 5000 update Max rise rate, 4.3.1 add immersion and repeat proof test to sequence, 4.7.3 update ATP manual operation check done with one hand using 30" head applied to both halves, and 4.7.4.2 remove high pressure test.
Standard

Coupling Assembly, Self-Sealing, One Side Only, Hydraulic

2019-01-10
CURRENT
AS1896B
This document establishes the requirements for aircraft, hydraulic couplings, self-sealing one side only, for use in Type II hydraulic systems (-65 to +275 °F temperature range) as defined by MIL-H-5440. The purpose being to connect a hose or tube to a standard MS33656, MS33514, or MIL-F-85421, or MIL-F-85720 fitting, and to provide the self-sealing feature on the hose or tube side of the connection.
Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification

2017-12-07
HISTORICAL
AS1650E
This SAE Aerospace Standard (AS) 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, and is designed for use from −65 to +400 °F and at 125 psig nominal operating pressure. AS1650 was not designed for the new certification requirements for flammable leakage zones and fuel tanks for lightning protection and assembly redundancy. As such their use and installation may require additional efforts and equipment to support new FAA CFR compliance. The AS7510 flexible coupling should be the preferred coupling for use in flammable leakage zones and fuel tanks that require service life and functionality for lightning protection and part redundancy.
Standard

Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification

2017-11-13
CURRENT
AS5420G
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems with an environmental operating temperature range of -65 °F (-54 °C) to +160 °F (+71 °C).
Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification

2016-02-26
HISTORICAL
AS1650C
This SAE Aerospace Standard (AS) 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, and is designed for use from 65 to +400 °F and at 125 psig nominal operating pressure.
Standard

Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification

2013-10-25
HISTORICAL
AS5420F
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems with an environmental operating temperature range of −65 °F (−54 °C) to +160 °F (+71 °C).
Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification

2010-08-24
HISTORICAL
AS1650B
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

Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification

2009-02-25
HISTORICAL
AS5420E
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems with an environmental operating temperature range of −65 °F (−54 °C) to +160 °F (+71 °C).
Standard

Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification

2008-08-21
HISTORICAL
AS5420D
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems with an environmental operating temperature range of −65 °F (−54 °C) to +160 °F (+71 °C).
Standard

Hose Assemblies, Metal, Medium Pressure, High Temperature

2007-12-03
CURRENT
AS1424G
This SAE Aerospace Standard (AS) covers medium-pressure, high-temperature, flexible, metal-hose assemblies suitable for operation in pneumatic systems up to 800 °F with excursion to 1200 °F for Class “B” and “N” and primarily for use on jet aircraft power plants. Refer to 1.2.1 for recommended usage.
Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement Specification

2006-09-11
HISTORICAL
AS5830
This aerospace specification defines the requirements for a threadless, flexible, conductive, self-bonding coupling assembly which, when installed on fixed cavity ferrules, provides a flexible, current carrying connection for joining tubing and components in aircraft fuel, vent and other systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for the service life of the aircraft system. The assembled coupling is for use from -65 to +200 °F at nominal operating pressures (125 psig for -08 through -64 and 30 psig for -72 through -88). This aerospace specification is a departure from prior qualification practices for assembled couplings. Prior practice sought to validate this type of assembled coupling design by conducting a sequence of tests on sets of coupling assemblies. There were multiple test sequences and each was conducted on a different set of coupling assemblies.
Standard

Hose Assemblies, Metal, Medium Pressure, High Temperature

2006-09-11
HISTORICAL
AS1424F
This SAE Aerospace Standard (AS) covers medium-pressure, high-temperature, flexible, metal-hose assemblies suitable for operation in pneumatic systems up to 800 °F with excursion to 1200 °F for Class “B” and “N” and primarily for use on jet aircraft power plants. Refer to 1.2.1 for recommended usage.
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, Hydraulic, Self-Sealing, Quick Disconnect

2004-05-04
CURRENT
AS25427
This specification covers the detail requirements for aircraft hydraulic self-sealing quick disconnect couplings, for use in types I and II hydraulic systems (-65°F to +275°F temperature range) as defined by Specification MIL-H-5440.
Standard

Hose Assemblies, Metal, Medium Pressure, High Temperature

2003-02-10
HISTORICAL
AS1424E
This SAE Aerospace Standard (AS) covers medium-pressure, high-temperature, flexible, metal-hose assemblies suitable for continuous operation in pneumatic systems up to 850 °F with short duration excursion to 1200 °F and primarily for use on jet aircraft power plants.
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