Standard
APPLICATION OF V-BAND COUPLINGS
2011-08-10
HISTORICAL
AIR869
Search Results
Standard
Adapter - Port Connection, Ring Locked Installation and Removal of
2017-03-01
CURRENT
MA2114B
This SAE Aerospace Standard provides the essential minimum design, installation and removal standard for MA2111, MA2112, MA2113, and MA2119 adapters, and is applicable when specified on engineering drawings or in procurement documents.
Standard
Adapters - Port Connection, Ring Locked Design, Installation and Removal of
2015-06-12
CURRENT
AS1301F
This SAE Aerospace Standard (AS) provides the essential minimum design, installation and removal standard for AS1299, AS1985, AS1986, AS4099, AS5368, and AS5986 adapters and is applicable when specified on engineering drawings or in procurement documents.
Standard
CLAMP, LOOP, TUBE 17-7PH CUSHION, SELF-LOCKING
2013-07-16
HISTORICAL
AS6264
Standard
CLAMP, LOOP, TUBE, 17-7PH, 275 °F, FUEL AND PETROLEUM BASED HYDRAULIC FLUID RESISTANT
2015-04-23
HISTORICAL
AS85052/1A
Standard
COUPLING ASSEMBLIES, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT 5000 and 8000 POUNDS PER SQUARE INCH, GAGE
2011-08-15
HISTORICAL
AS4157
This specification covers the requirements for Aircraft Hydraulic, Self-Sealing, Quick Disconnect Couplings for use in 5000 and 8000 lbf/in2 (gage) lightweight hydraulic systems.
Standard
COUPLING ASSEMBLIES, NON-LOCKING PROBE STYLE, MINIATURE SELF-ALIGNING, SELF-SEALING DISCONNECTS
1996-11-01
HISTORICAL
AS5072
This SAE Aerospace Standard (AS) establishes the general requirements for a miniature probe type self-sealing, self-aligning, non-locking coupling intended for aerospace liquid cooling systems. The AS5072/slash sheets define the specific performance and dimensional requirements.
Standard
COUPLING ASSEMBLIES, NON-LOCKING PROBE STYLE, MINIATURE SELF-ALIGNING, SELF-SEALING DISCONNECTS
1997-06-01
HISTORICAL
AS5072A
This SAE Aerospace Standard (AS) establishes the general requirements for a miniature probe type self-sealing, self-aligning, non-locking coupling intended for aerospace liquid cooling systems. The AS5072/slash sheets define the specific performance and dimensional requirements.
Standard
COUPLING ASSEMBLY, SELF-SEALING, ONE SIDE ONLY, HYDRAULIC
1984-09-01
HISTORICAL
AS1896
This specification covers the requirements for aircraft, hydraulic couplings, self sealing one side only, for use in Type II hydraulic systems (-65°F to +275° 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 fitting and provide the self sealing feature on that side only.
Standard
Coupling Assemblies, Hydraulic, Self-Sealing, Quick Disconnect 5000 and 8000 Pounds Per Square Inch, Gage
2015-06-30
HISTORICAL
AS4157A
This specification covers the requirements for aircraft hydraulic, self-sealing, quick disconnect couplings for use in 5000 and 8000 lbf/in2 (gage) lightweight hydraulic systems.
Standard
Coupling Assemblies, Hydraulic, Self-Sealing, Quick Disconnect 8000 Pounds Per Square Inch, Gage
2017-09-07
CURRENT
AS4157B
This specification covers the requirements for aircraft hydraulic, self-sealing, quick disconnect couplings for use in 8000 lbf/in2 (gage) lightweight hydraulic systems.
Standard
Coupling Assemblies, Non-Locking Probe Style, Miniature Self-Aligning, Self-Sealing Disconnects
1998-01-01
HISTORICAL
AS5072B
This SAE Aerospace Standard (AS) establishes the general requirements for a miniature probe type self-sealing, self-aligning, non-locking coupling intended for aerospace liquid cooling systems. The AS5072/slash sheets define the specific performance and dimensional requirements.
Standard
Coupling Assemblies, Non-Locking Probe Style, Miniature Self-Aligning, Self-Sealing Disconnects
2013-01-07
CURRENT
AS5072C
This SAE Aerospace Standard (AS) establishes the general requirements for a miniature probe type self-sealing, self-aligning, non-locking coupling intended for aerospace liquid cooling systems. The AS5072/slash sheets define the specific performance and dimensional requirements.
Standard
Coupling Assemblies, Quick Disconnect, Automatic Shutoff
2019-04-23
CURRENT
AS7413A
This specification establishes requirements for automatic shutoff, quick-disconnect coupling assemblies for fuel and oil lines.
Standard
Coupling Assemblies, Quick Disconnect, Automatic Shutoff
2011-06-08
HISTORICAL
AS7413
This specification establishes requirements for automatic shutoff, quick-disconnect coupling assemblies for fuel and oil lines.
Standard
Coupling Assembly, Hydraulic Self Sealing, Quick Disconnect
2013-01-02
HISTORICAL
ARP1709
This specification covers the requirements for aircraft, hydraulic, self sealing, quick disconnect couplings, for use in type II hydraulic systems (-65°F to +275°F temperature range) as defined by MIL-H-5440.
Standard
Coupling Assembly, Self-Sealing, One Side Only, Hydraulic
2013-01-02
HISTORICAL
AS1896A
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, 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
Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
2017-07-10
HISTORICAL
AS1650D
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.
