Standard
NUT - HEX, PORT FITTING CONNECTOR, AMS5639, MJ THREAD, METRIC
2023-09-01
CURRENT
MA2521A
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Standard
NUT - HEX, BACK-UP RING, PORT FITTING CONNECTOR, AMS5639, MJ THREAD, METRIC
2023-09-01
CURRENT
MA2520A
Standard
Torsion Strength Testing of Hydraulic Tube Joints
2023-07-06
CURRENT
ARP4457A
This Aerospace Recommended Practice (ARP) establishes uniform requirements and procedures to determine the torsional strength of permanent hydraulic tube joints. It also establishes testing equipment and apparatus for torsion testing.
Standard
Trademarks, Hydraulic System Component Manufacturers, Index of
2022-12-20
CURRENT
AIR1973B
This index of trademarks of current and former manufacturers of aerospace fittings, couplings, hoses, and tube support devices is within the scope of activities of the SAE G-3 Committee and available at the time of publication. Supplier markings from previous publication are maintained for component traceability. Suggestions for additional entries or corrections shall be sent to SAE in Warrendale, PA.
Standard
FITTING END ASSEMBLY, INTERNAL THREAD, RETAINED NUT, BEAM SEAL, DESIGN STANDARD
2022-08-05
CURRENT
AS4209E
Standard
PORT-FLUID CONNECTION, RING LOCKED INSERT, STANDARD DIMENSIONS FOR
2022-05-09
CURRENT
AS1958A
Standard
T-Bolt and Eye Bolt, A286 CRES, 1000 °F Fatigue Rated
2021-09-01
CURRENT
AS4108D
This specification defines the requirements for A286 CRES T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings at 1000 °F maximum ambient temperature.
Standard
TUBE END - BEADED, DESIGN STANDARD
2020-12-10
CURRENT
AS5131A
Standard
FITTING END ASSEMBLY, INTERNAL THREAD, RETAINED NUT, BEAM SEAL, DESIGN STANDARD
2020-09-18
HISTORICAL
AS4209D
Standard
Clamp Assembly, Saddle Type, Cushioned, General Specification For
2020-04-21
CURRENT
AS85449B
This SAE Aerospace Standard (AS) defines the requirements for saddle-type clamps. Tests and criteria noted do not indicate any specific areas of application or usage. Supplemental testing may be necessary to determine suitability for specific environments and applications.
Standard
Hose Assembly, Type Classifications of, Basic Performance and Fire Resistance
2020-02-14
WIP
AS150G
This SAE Aerospace Standard (AS) establishes Type classification for those hose assemblies commonly used in aerospace fuel, lubricating oil, and hydraulic fluid systems.
Standard
Service Damage Limits for Aircraft Hydraulic Tubing
2019-10-09
WIP
AIR1388C
This SAE Aerospace Information Report (AIR) is intended to assist in evaluating the serviceability of damaged hydraulic tubing lines. The performance requirements are outlined to which the defect sample were tested. Test methods and data are described and summarized. Permissible defect limits are listed for 6061-T6 aluminum return lines, 3000 psi hydraulic tubing of 21Cr-6Ni-9Mn SS, 304 1/8 hard, corrosion resistant steel (CRES), as well as 3Al-2.5V CWRS and 3Al-2.5V annealed, seamless titanium tubing. All dimensions are in inches unless otherwise noted.
Standard
Clamp Material, Injection Molded
2019-09-26
CURRENT
AIR1397B
This report presents the material properties and test requirements for an injection molded thermoplastic compound utilized for fabrication of AS1396 clamp block assembly.
Standard
Titanium Hydraulic Tubing, Ti-3Al-2.5V Cold Worked and Stress Relieved, Up to 35000 kPa (5080 psi), Requirements for Qualification Testing and Control
2019-06-04
CURRENT
AS5620C
This SAE Aerospace Standard (AS) shall be used in conjunction with AMS4946 to provide requirements for qualification testing and for qualified products listing (QPL) and qualified manufacturer listing (QML) for Ti-3Al-2.5V cold worked and stress relieved hydraulic system tubing. The basic tubing shall comply with the requirements of AMS4946.
Standard
Lubricant Application, Solid Film, Heat Cured, Potable Water, Hydraulic, and Other Fluid Systems
2019-05-20
CURRENT
AS6450B
This SAE Aerospace Standard (AS) establishes the surface pretreatment, temperature, and baking time required to cure AS6449 Type I and Type II solid film lubricant (SFL) when it is applied over the surfaces of manufactured parts of various metals. Application method may be dipping or spraying.
Standard
Clamp Selection and Installation Guide
2019-05-20
CURRENT
ARP1897A
This document is prepared as an aid in the selection of clamping devices and their use in aerospace equipment for the installation and support of tubing and wiring. For recommended installation practices, refer to ARP994.
Standard
Standard Words for Test Paragraphs for Tube Fittings and Tube Assemblies
2019-04-30
CURRENT
AIR1378C
This Aerospace Information Report (AIR) is written as a guide for the wording recommended for use, when applicable, in design and procurement specifications for tube fittings and tube assemblies, both for general aerospace fluid power applications and for specific applications.
Standard
Flexure Testing of Hydraulic Tubing Joints and Fittings
2019-04-23
CURRENT
ARP1185C
This SAE Aerospace Recommended Practice (ARP) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure tests of fittings and joints for hydraulic tubing materials such as AMS 5561 (21Cr-6Ni-9Mn) steel or AMS 4944 (3AL-2.5V) titanium. A mean stress is applied by holding system pressure in the specimens and flexing in a rotary or planar bending test machine.
Standard
Fittings, Weld, Fluid Connection, 5000 psi Maximum
2019-03-26
CURRENT
AS4510A
This SAE Aerospace Standard (AS) establishes the requirements for weld fluid connection fittings and rings to be orbital arc welded to tubing for use in aircraft fluid systems up to a maximum operating pressure of 5000 psi.
Standard
Fittings, Weld to Beam, Seal, Fluid Connection
2019-03-20
CURRENT
AS4510/2A
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both weld fitting end and beam seal fitting end connections for use in all types of fluid systems.
