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
CURRENT
ARP605
Standard
Hose Assemblies: Pneumatic, Aircraft and Missiles, High Temperature, High Pressure
2002-12-16
CURRENT
ARP615
Standard
Hose Assemblies: Pneumatic, Aircraft and Missiles, High Temperature, Medium Pressure
2002-12-16
CURRENT
ARP609
Standard
Hose Assemblies: Aircraft and Missiles, Light-Weight Plastic Hose, Low Pressure
2002-12-16
CURRENT
ARP1180
Standard
High Pressure Compressed Gas Hose Assemblies for Aircraft and Missile Ground Support Equipment
2002-12-16
CURRENT
AS608
Standard
Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft, Metric (Supplement 1)
2017-04-18
CURRENT
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
HISTORICAL
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
CURRENT
MA2024
Standard
GASKET, FITTING END, 24° CONE
2015-04-21
CURRENT
AS4825
Standard
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems (Supplement 1)
2013-01-02
CURRENT
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
CURRENT
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
Titles, SAE Subcommittee G-3E Aerospace Tubing Installation Documents, Selection Of
2013-01-02
CURRENT
ARP1987/3
The scope of this SAE Aerospace Recommended Practice (ARP) is to establish the procedure for creating titles of aerospace tubing and clamp installation documents generated by SAE Subcommittee G-3E.
Standard
Standardization, Hydraulic Tube Walls
2013-01-07
CURRENT
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
CURRENT
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
HISTORICAL
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
HISTORICAL
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
CURRENT
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
HISTORICAL
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
FITTING, ELBOW, 90°, STANDARD AND REDUCER FLARELESS TUBE TO PIPE, EXTERNAL THREAD
2007-08-21
HISTORICAL
AS897B
