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
Fittings, Flanged to Beaded, Fluid Connection
2015-07-27
HISTORICAL
AS4875/2
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both flanged fitting ends and beaded hose connections for use in all types of fluid systems.
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
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
PACKING, PREFORMED, AIR DUCT HOSE, GROUND COOLING
2013-01-07
CURRENT
AS38386/3
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
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
Qualification of Hydraulic Tube Joints to Specified Flexure Fatigue Requirements
2019-01-03
WIP
ARP1258C
This SAE Aerospace Recommended Practice (ARP) establishes the method for qualification testing of tube joints and fitting attachments, using the flexure test method described in ARP1185. This qualification test method allows the determination of S-N type stress versus cycles or D-N type deflection versus cycles curves, as illustrated in AIR1418 as an alternate to flexure testing to a minimum endurance stress level.
Standard
Qualification of Hydraulic Tube Joints to Specified Flexure Fatigue Requirements
2013-01-02
CURRENT
ARP1258B
This SAE Aerospace Recommended Practice (ARP) establishes the method for qualification testing of tube joints and fitting attachments, using the flexure test method described in ARP1185. This qualification test method allows the determination of S-N type stress versus cycles or D-N type deflection versus cycles curves, as illustrated in ARP1418 as an alternate to flexture testing to a minimum endurance stress level.
Standard
PRESTRESSING (AUTOFRETTAGING) OF HYDRAULIC TUBING LINES
1977-07-01
HISTORICAL
AIR1379
This AIR is intended to describe and document a process presently in use for proof testing, which at the same time improves the fatigue life of 304 1/8 hard CRES and 3A1-2.5V CWSR titanium hydraulic tubing lines.
Standard
Prestressing (Autofrettaging) of Hydraulic Tubing Lines
2013-01-02
HISTORICAL
AIR1379A
This AIR is intended to describe and document a process presently in use for proof testing, which at the same time improves the fatigue life of 304 1/8 hard CRES and 3Al-2.5V CWSR titanium hydraulic tubing lines.
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.
