Search Results

Standard

Torsion Strength Testing of Hydraulic Tube Joints

2013-01-02

HISTORICAL

ARP4457

This Aerospace Recommended Practice (ARP) establishes uniform requirements and procedures to determine the torsional strength of permanent hydraulic tube joints. It also establishes testing equipment and apparatus for torsion testing.

Standard

Clamp Loads and Bending Stresses in Aircraft Tubing Installations

2013-01-02

HISTORICAL

AIR1593

This Aerospace Information Report (AIR) contains information relative to stresses and loads developed in tubes, fittings and clamps caused by tube deflections encountered in misaligned installations.

Standard

Clamp Loads and Bending Stresses in Aircraft Tubing Installations

2020-10-09

CURRENT

AIR1593A

This SAE Aerospace Information Report (AIR) contains information relative to stresses and loads developed in tubes caused by tube deflections encountered in misaligned installations. Users are advised that when calculating the stresses and loads of a tubing system, the yield strength of existing loop clamp material is significantly lower than the tubing materials specified herein and should be considered.

Standard

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

2006-09-07

HISTORICAL

AS5951A

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, para-aramid 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

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

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

2015-07-27

HISTORICAL

AS5951C

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, para-aramid 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

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

2006-11-07

HISTORICAL

AS5951B

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, para-aramid 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

Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems

2017-02-22

CURRENT

AS5951D

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, para-aramid reinforced, hose assemblies suitable for use in 275 °F (135 °C), 5080 psi (35000 kPa) aircraft hydraulic systems.

Standard

Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft (Supplement 1)

2013-01-09

CURRENT

AS620SUP1

This supplement forms a part of Aerospace Standard AS620, HOSE ASSEMBLIES, CONVOLUTED, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT, and shall be used to identify hose assembly standards citing this procurement specification.

Standard

Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems

2019-04-11

CURRENT

AS5960C

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35000 kPa) aircraft hydraulic systems.

Standard

Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems

2013-03-07

HISTORICAL

AS5960B

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35 000 kPa) aircraft hydraulic systems. NOTE: The SI metric units defined herein are soft conversion units.

Standard

Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems

2008-07-15

HISTORICAL

AS5960A

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35 000 kPa) aircraft hydraulic systems. NOTE: The SI metric units defined herein are soft conversion units.

Standard

Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems

2004-07-28

HISTORICAL

AS5960

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35 000 kPa) aircraft hydraulic systems. NOTE: The SI metric units defined herein are soft conversion units.

Standard

CLAMP, LOOP, TUBE, 17-7PH, 275 °F, FUEL AND PETROLEUM BASED HYDRAULIC FLUID RESISTANT

2015-04-23

HISTORICAL

AS85052/1A

Standard

NUT - HEX, PORT FITTING CONNECTOR, AMS5639, MJ THREAD, METRIC

2023-09-01

CURRENT

MA2521A

Standard

NUT - HEX, BACK-UP RING, PORT FITTING CONNECTOR, AMS5639, MJ THREAD, METRIC

2023-09-01

CURRENT

MA2520A

Standard

Fittings, Lubrication

2001-05-01

HISTORICAL

AS35411

This SAE Aerospace Standard (AS) covers the requirements for threaded lubrication fittings, straights and elbows, to be used for admitting and retaining lubricants supplied by pressure lubricating equipment.

Standard

Marking; Standard Hose, Aircraft

2023-09-11

CURRENT

ARP6002A

This document establishes the industry standard practices for marking standard elastomeric hose used in aircraft manufacture and repair.

Standard

Missile and Rocket Applications: Hose Assemblies, Flexible Metal, High Pressure and High Temperature

2023-10-02

CURRENT

ARP907A

This recommended practice covers the requirements and qualification tests for two types of flexible all-metal hose assemblies intended for hydraulic use on missile and rocket applications at rated pressures of 4000 psi. Type I -65° to +650 °F service temperature range Type II -65° to +1000 °F service temperature range

Standard

CLAMP, LOOP, TUBE 17-7PH CUSHION, SELF-LOCKING

2013-07-16

HISTORICAL

AS6264