Standard
ALTERNATE DIMENSIONS, CENTER BODY SECTION, SHAPE FLUID FITTING, DESIGN STANDARD
2018-02-11
CURRENT
AS1376E
Search Results
Standard
APPLICATION OF V-BAND COUPLINGS
2011-08-10
HISTORICAL
AIR869
Standard
AS5177 Cap Assy
2008-03-08
WIP
AS5177A
Prepare AS replacement standard for MIL-F-5509 flared fitting
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
Aluminum Fittings, Axially Swaged Tube with Flareless Separable, Fluid System Up to 1500 psi (10 340 kPa) Maximum, Specification for
2011-11-09
HISTORICAL
AS6116
This SAE Aerospace Standard (AS) establishes the requirements for externally swaged aluminum tube fittings on aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems including pneumatic, coolants, and fire extinguishers up to a maximum operating pressure of 1500 psig (10 340 kPa) and a maximum operating temperature range of −65 to +225 °F (−54 to +107 °C). This specification covers a common aluminum fitting that may be used for a range of operating pressures up to 1500 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS6124. Table 12 shows applicable aerospace fitting part number standard and tubing materials and operating pressures.
Standard
Aluminum Fittings, Axially Swaged Tube with Flareless Separable, Fluid System Up to 1500 psi (10340 kPa) Maximum, Specification for
2016-10-17
CURRENT
AS6116A
This SAE Aerospace Standard (AS) establishes the requirements for externally swaged aluminum tube fittings on aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems including pneumatic, coolants, and fire extinguishers up to a maximum operating pressure of 1500 psig (10340 kPa) and a maximum operating temperature range of -65 to +225 °F (-54 to +107 °C). This specification covers a common aluminum fitting that may be used for a range of operating pressures up to 1500 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS6124. Table 12 shows applicable aerospace fitting part number standard and tubing materials and operating pressures.
Standard
BENDING RADIUS, TUBE (Aircraft Engine)
1943-03-01
HISTORICAL
AS130
Standard
BOLT, CLUSTER FITTING, SINGLE PORT FLARELESS
2007-11-05
HISTORICAL
AS21938A
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
CLAMP, RECTANGULAR, 2 PIECE, CUSHIONED, WITH WEDGES, HYDROCARBON FLUID RESISTANT, METRIC
2015-04-27
CURRENT
MA2154/1
Standard
COLOR CODING - ELASTOMERS FOR TUBE CLAMP CUSHIONS
1991-07-01
HISTORICAL
ARP1527A
This Aerospace Recommended Practice (ARP) establishes uniform requirements for color coding of elastomeric cushions on clamps used in aerospace tubing systems, wire bundle retention, and similar applications.
Standard
COLOR CODING - ELASTOMERS FOR TUBE CLAMP CUSHIONS
1980-03-01
HISTORICAL
ARP1527
This Aerospace Recommended Practice (ARP) establishes uniform requirements for color coding of elastomeric cushions on clamps used in aerospace tubing systems, wire bundle retention, and similar applications.
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
Clamp Loads and Bending Stresses in Aircraft Tubing Installations
2013-01-02
HISTORICAL
AIR1593
This Aerospace Information Report (AIR) contains information relative to stresses and loads developed in tubes, fittings and clamps caused by tube deflections encountered in misaligned installations.
Standard
Clamp Loads and Bending Stresses in Aircraft Tubing Installations
2020-10-09
CURRENT
AIR1593A
This SAE Aerospace Information Report (AIR) contains information relative to stresses and loads developed in tubes caused by tube deflections encountered in misaligned installations. Users are advised that when calculating the stresses and loads of a tubing system, the yield strength of existing loop clamp material is significantly lower than the tubing materials specified herein and should be considered.
