Standard
AS5177 Cap Assy
2008-03-08
WIP
AS5177A
Prepare AS replacement standard for MIL-F-5509 flared fitting
Search Results
Standard
Routine Inspection and Test Procedures for Aircraft Refueling Hoses
2002-12-16
ARP605
Standard
Hose Assemblies: Pneumatic, Aircraft and Missiles, High Temperature, High Pressure
2002-12-16
ARP615
Standard
Hose Assemblies: Pneumatic, Aircraft and Missiles, High Temperature, Medium Pressure
2002-12-16
ARP609
Standard
Hose Assemblies: Aircraft and Missiles, Light-Weight Plastic Hose, Low Pressure
2002-12-16
ARP1180
Standard
High Pressure Compressed Gas Hose Assemblies for Aircraft and Missile Ground Support Equipment
2002-12-16
AS608
Standard
Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft, Metric (Supplement 1)
2017-04-18
MA620SUP1A
This supplement forms a part of Aerospace Standard MA620, HOSE ASSEMBLIES, CONVOLUTED, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT, METRIC and shall be used to identify hose assembly standards citing this procurement specification.
Standard
Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft, Metric (Supplement 1)
2004-06-25
MA620SUP1
This supplement forms a part of Aerospace Standard MA620, HOSE ASSEMBLIES, CONVOLUTED, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT, METRIC and shall be used to identify hose assembly standards citing this procurement specification.
Standard
FLANGE PROFILES, V-COUPLING, DESIGN STANDARD, METRIC
2015-04-24
MA2024
Standard
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems (Supplement 1)
2013-01-02
AS1975SUP1
This supplement forms a part of AS1975, Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems and shall be used to identify hose assembly standards citing this procurement specification.
Standard
Industry Practices and Guidelines for the Selection of Coiled Tubes, Flexible Hoses, Swivels, and Extension Fittings for Aircraft Fluid Systems
2013-01-02
AIR4918
To present a summary of the guidelines and practices presently being used by the aerospace industry for the selection of coiled tubes, flexible hoses, swivel fittings, and extension fittings in aircraft fluid systems.
Standard
Standardization, Hydraulic Tube Walls
2013-01-07
AS4467
This SAE Aerospace Standard (AS) defines a series of standardized tube walls to be used for high pressure hydraulic tubing. These tube walls are applicable to all homogenous tube materials (i.e., aluminum, steel, titanium) throughout a rated pressure range of 1000 to 8000 psi and a maximum rated operating temperature range of 160 to 450 °F. All future aerospace applications for which a required tube outside diameter/tube wall combination is not presently available shall be selected from the table contained herein (see Figure 1).
Standard
Investigation of PTFE "Melt" Phenomenon for High Pressure Hoses
2021-03-16
AIR4092B
To provide information regarding a unique failure mode and alternate solutions for consideration by application designers.
Standard
Flexure Fatigue Strength of Tube Fitting Joints
2013-01-02
AIR1418A
This SAE Aerospace Information Report (AIR) presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S versus number of cycles to failure N. The graphs have been prepared from data obtained by actual testing conducted in accordance with ARP1185.
Standard
FLEXURE FATIGUE STRENGTH OF TUBE FITTING JOINTS
2011-08-09
AIR1418
This information report presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S vs. number of cycles to failure N. The graphs have been prepared from data obtained by actual testing conducted in accordance with ARP 1185.
Standard
Flexure Fatigue Strength of Tube Fitting Joints
2020-05-06
AIR1418B
This SAE Aerospace Information Report (AIR) presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S versus number of cycles to failure N. The graphs have been prepared from data obtained by actual testing conducted in accordance with ARP1185.
Standard
Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35 000 kPa), Specification for
2010-07-07
AS5000C
This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone AS5827 or EN 6123 flareless Ring locked fitting assemblies per AS5550 and AS5865, for use in aircraft fluid systems at nominal operating pressure of 5080 psi (35 000 kPa) maximum and operating temperature range of -65 to +275 °F (-54 to +135 °C). The general requirements shall be for, but not limited to, commercial aircraft hydraulic components per AS4941, using port configuration as specified in AS5551.
Standard
FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS
1973-12-01
ARP1185
This recommended practice 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 AM 350, 21Cr-6Ni-9Mn steel, or 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
FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS
2011-08-10
ARP1185A
This Aerospace Recommended Practice 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 AM 350, 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. Flexure testing of metric tubing joints and fittings is covered by MA 2003.
Standard
Trademarks, Hydraulic System Component Manufacturers, Index of
2013-01-02
AIR1973A
This index of trademarks of current and former manufacturers of aerospace fittings, couplings, hose, and tube support devices is within the scope of activities of the SAE G-3 Committee and available at the time of publication. Suggestions for additional entries may be sent to the SAE in Warrendale, PA.
