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
Impulse Test Equipment
1960-03-01
HISTORICAL
ARP603
This recommended practice covers design schematics of two test machines capable of producing hydraulic impulse pressure cycles with a maximum operating pressure of 5000 psi.
Standard
IMPULSE TEST EQUIPMENT FOR TESTING HYDRAULIC SYSTEM COMPONENTS
1963-09-01
HISTORICAL
ARP603A
This recommended practice covers design schematics of two test machines capable of producing hydraulic impulse pressure cycles with a maximum operating pressure of 5000 psi.
Standard
IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES
2007-01-17
HISTORICAL
ARP603F
This Aerospace Recommended Practice (ARP) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
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
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
HOSE ASSEMBLY TETRAFLUOROETHYLENE, HEAVY DUTY, HIGH TEMPERATURE, HIGH PRESSURE, 4,000 PSI (27,580 kPa) HYDRAULIC AND PNEUMATIC
1984-05-01
HISTORICAL
AS614
This specification defines the requirements for heavy duty hose assemblies suitable for use in high temperature, high-pressure, 4000 psi (27,584 kPa), aircraft and missile hydraulic fluid systems.
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.
