Search Results

Standard

HOSE, POLYTETRAFLUOROETHYLENE TFE Fluorocarbon Resin Wire Braid Reinforced

1974-12-01

HISTORICAL

AMS3380B

This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible hose reinforced with wire braid.

Standard

Hose, Polytetrafluoroethylene TFE Fluorocarbon Resin Wire Braid Reinforced

2012-12-11

HISTORICAL

AMS3380D

This specification covers a polytetrafluoroethylene resin in the form of extruded and sintered flexible tube reinforced with wire braid.

Standard

HOSE, POLYTETRAFLUOROETHYLENE TFE Fluorocarbon Resin Wire Braid Reinforced

1983-07-01

HISTORICAL

AMS3380C

This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible hose reinforced with wire braid.

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

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

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

HOSE ASSEMBLY, TETRAFLUOROETHYLENE, LIGHTWEIGHT, 204°C, 21 000 kPa HYDRAULIC, METRIC

1983-07-01

HISTORICAL

MA2007

This specification covers lightweight hose assemblies intended for use in high-temperature, 204°C, high-pressure, 21 000 kPa (210 bar) aircraft hydraulic systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall.

Standard

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED HEAVY-DUTY, 275 °F 3000 psi, AIRCRAFT HYDRAULIC SYSTEMS

1992-06-15

HISTORICAL

AS4623

This document defines the requirements for heavy-duty hose assemblies suitable for use in 275 °F, 3000 psi aircraft systems where rapid rate pressure pulsing and torsional/longitudinal flexing may occur in addition to normal hydraulic system loading.

Standard

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED HEAVY-DUTY, 275 °F 3000 psi, AIRCRAFT HYDRAULIC SYSTEMS

1995-09-01

HISTORICAL

AS4623A

This document defines the requirements for heavy-duty polytetrafluoroethylene (PTFE) lined, para-aramid reinforced, hose assembly suitable for use in 275 °F, 3000 psi aircraft systems where rapid rate pressure pulsing and torsional/longitudinal flexing may occur in addition to normal hydraulic system loading. Size -16 and -20 are limited to +225 °F service.

Standard

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), WIRE REINFORCED 204 °C, 28 000 kPa, HYDRAULIC, METRIC

1994-01-01

HISTORICAL

MA614

This SAE Aerospace Standard establishes the requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aerospace hydraulic systems at temperatures between -55 °C and 204 °C and at a nominal pressure up to 28 000 kPa (280 bar). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated. The use of these hose assemblies in high pressure pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this document, for example, oxygen, shall be subject to the approval of the purchaser.

Standard

Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems

2007-01-19

HISTORICAL

AS1975C

This Aerospace Standard (AS) defines the requirements for a polytetrafluoroethylene (PTFE) lined, para-aramid fiber reinforced, hose assembly suitable for use up to 4000 psi, and up to 275 °F, aircraft and missile hydraulic and pneumatic systems.

Standard

HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 275 °F, STANDARD DUTY, 4000/3000 psi, HYDRAULIC, AIRCRAFT SYSTEMS

1994-07-01

HISTORICAL

AS1975B

This document defines the requirements for a PTFE lined, aramid reinforced assembly suitable for use up to 275 °F and up to 4000 psi aircraft and missile hydraulic and pneumatic systems.

Standard

HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 275 °F, STANDARD DUTY, 4000/3000 lbf/in2, HYDRAULIC, AIRCRAFT SYSTEMS

1992-06-01

HISTORICAL

AS1975A

This document defines the requirements for a PTFE lined, aramid reinforced assembly suitable for use up to 275 °F and up to 4000 lbf/in2 aircraft and missile hydraulic and pneumatic systems.

Standard

Coupling Assemblies, Non-Locking Probe Style, Miniature Self-Aligning, Self-Sealing Disconnects

1998-01-01

HISTORICAL

AS5072B

This SAE Aerospace Standard (AS) establishes the general requirements for a miniature probe type self-sealing, self-aligning, non-locking coupling intended for aerospace liquid cooling systems. The AS5072/slash sheets define the specific performance and dimensional requirements.

Standard

Coupling Assemblies, Non-Locking Probe Style, Miniature Self-Aligning, Self-Sealing Disconnects

2013-01-07

CURRENT

AS5072C

This SAE Aerospace Standard (AS) establishes the general requirements for a miniature probe type self-sealing, self-aligning, non-locking coupling intended for aerospace liquid cooling systems. The AS5072/slash sheets define the specific performance and dimensional requirements.

Standard

COUPLING ASSEMBLIES, NON-LOCKING PROBE STYLE, MINIATURE SELF-ALIGNING, SELF-SEALING DISCONNECTS

1997-06-01

HISTORICAL

AS5072A

This SAE Aerospace Standard (AS) establishes the general requirements for a miniature probe type self-sealing, self-aligning, non-locking coupling intended for aerospace liquid cooling systems. The AS5072/slash sheets define the specific performance and dimensional requirements.

Standard

Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35,000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems

2004-09-08

HISTORICAL

AS5951

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, paraaramid reinforced, hose assemblies suitable for use in 275 °F (135 °C), 5080 psi (35,000 kPa) aircraft hydraulic systems. NOTE: The SI metric units defined herein are soft conversion units.

Standard

Drawing Interpretation and Standard Machining Practices, Couplings, Fittings, and Hose Ends, Fluid Systems

2023-06-02

CURRENT

AS4296A

This SAE Aerospace Standard (AS) provides general information for the interpretation and clarification of engineering drawing requirements relating to the manufacture and inspection of fluid system couplings, tube fittings, and hose ends. Because it is impractical to define every minute detail of the part on the face of the drawing, this standard describes interpretations of dimensioning of general machining features and otherwise undefined tolerances that fall under the heading of “good shop practice.” This standard is supplemental to ASME Y14.5M-1994 and explains, defines, and interprets drawing terms or practices that are not addressed by ASME Y14.5M-1994. Unless otherwise specified in this standard, drawing interpretations contained in ASME Y14.5M-1994 shall apply.