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
Hose and Hose Assembly Selection, Installation, Inspection and Maintenance Guidelines, Listing of
2022-02-02
CURRENT
AIR5386A
This SAE Aerospace Information Report (AIR) applies as general guidance to users of all hose and hose assembly types used in aerospace applications. See 6.4 for similar guidance for non-aerospace applications.
Standard
Hose and Hose Assembly Selection, Installation, Inspection and Maintenance Guidelines, Listing of
2013-01-02
HISTORICAL
AIR5386
This SAE Aerospace Information Report (AIR) applies as general guidance to users of all hose and hose assembly types used in aerospace applications. See 6.4 for similar guidance for non-aerospace applications.
Standard
IMPULSE TESTING OF HYDRAULIC HOSE ASSEMBLIES, TUBING, AND FITTINGS
1977-10-01
HISTORICAL
ARP603D
This recommended practice establishes the requirements and the procedures for impulse testing of hose assemblies, tubing, and fittings for use in aerospace hydraulic systems of 4000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
Standard
IMPULSE TESTING OF HYDRAULIC HOSE ASSEMBLIES, TUBING, AND FITTINGS
1979-08-01
HISTORICAL
ARP603E
This Aerospace Recommended Practice (ARP) establishes the requirements and the procedures for impulse testing of hose assemblies, tubing, and fittings for use in aerospace hydraulic systems of 4000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
Standard
IMPULSE TESTING OF HYDRAULIC HOSE ASSEMBLIES, TUBING, AND FITTINGS
1975-07-15
HISTORICAL
ARP603C
This recommended practice establishes the requirements and the procedures for impulse testing of hose assemblies, tubing, and fittings for use in aerospace hydraulic systems of 3000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
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
Hose, Rubber, Wire-Wound, Synthetic, Ice Eliminating System
2013-01-09
CURRENT
AS6399
This document establishes the requirements for a lightweight, nonkink, flexible elastomeric hose. This hose is typically used with air-operated aircraft ice-preventive systems.
Standard
Test Methods for Tube-Fitting Assemblies, Metric (ISO 10583)
2015-08-21
CURRENT
MA2094
This SAE Aerospace Standard (AS) specifies test methods for fitting assemblies used in aircraft fluid systems in the pressure classes B, D, and E, and in temperature Types I, II, and III of MA 2001. This document applies each time that it is referred to in a procurement specification or other definition document. Fluids and materials used for the tests are listed in Section 2.
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).
