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2016-05-19
WIP Standard
AS1650D
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, and is designed for use from 65 to +400 °F and at 125 psig nominal operating pressure.
2016-05-02
Standard
AS4130C
SCOPE IS UNAVAILABLE.
2016-05-02
Standard
AS4134C
SCOPE IS UNAVAILABLE.
2016-05-02
Standard
AS4136C
SCOPE IS UNAVAILABLE.
2016-05-02
Standard
AS1975G
This SAE 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.
2016-04-21
WIP Standard
AS1043G
No scope available.
2016-04-20
Standard
AS4859B
SCOPE IS UNAVAILABLE.
2016-04-20
Standard
AS4861B
SCOPE IS UNAVAILABLE.
2016-04-20
Standard
AS21916E
SCOPE IS UNAVAILABLE.
2016-04-15
Standard
AS1718E
SCOPE IS UNAVAILABLE.
2016-04-13
Standard
AS1895D
This SAE Aerospace Standard establishes the requirements for a V-retainer coupling, flanges, and seal suitable for joining high pressure and high temperature ducting in aircraft bleed air systems. The rigid coupling joint assembly, hereafter referred to as “the joint”, shall operate within the temperature range of -65 to +1200 °F.
2016-04-13
Standard
AS1895/7D
SCOPE IS UNAVAILABLE.
2016-04-08
WIP Standard
AS6121D
SCOPE IS UNAVAILABLE.
2016-04-07
Standard
AS1007J
SCOPE IS UNAVAILABLE.
2016-04-07
Standard
AS21913E
SCOPE IS UNAVAILABLE.
2016-04-07
Standard
AS21915D
SCOPE IS UNAVAILABLE.
2016-03-08
WIP Standard
AS6368
Establish a design standard for the High-Beam, All-Metal Self-Locking Hexagon Nuts that are used on the T-Bolts that tighten V-Band Couplings, band clamps and strap assemblies. This standard to include: drawing, dimensions, materials, manufacturing processes, and part number code system.
2016-03-05
Standard
AS6121C
SCOPE IS UNAVAILABLE.
2016-03-01
WIP Standard
AS6367
Establish a general specification for the High-Beam, All-Metal Self-Locking Hexagon Nuts that are used on the T-Bolts that tighten V-Band Couplings, band clamps and strap assemblies
2016-02-26
Standard
AS1650C
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, and is designed for use from 65 to +400 °F and at 125 psig nominal operating pressure.
2016-02-24
WIP Standard
AS620H
This SAE Aerospace Standard (AS) defines the requirements for a convoluted polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in aircraft fluid systems at temperatures of -65 to 400 °F and at operating pressures per Table 1.
2016-02-24
WIP Standard
AS614D
This Aerospace Standard (AS) defines the requirements for a heavy duty polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, high pressure, 4000 psi, aircraft and missle hydraulic fluid systems.
2016-02-24
WIP Standard
AS604F
This Aerospace Standard (AS) defines the requirements for a heavy braid polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, 400 °F, high pressure, 3000 psi, aircraft hydraulic fluid systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall. The -20 size operating temperature is limited to 275 °F maximum.
2016-02-24
Standard
AS6322
SCOPE IS UNAVAILABLE.
2016-02-23
WIP Standard
AS1472B
This specification covers three types of lightweight, low pressure, wire and/or fabric reinforced hose assemblies primarily for use in aircraft potable water systems.
2016-02-22
WIP Standard
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 (35 000 kPa) aircraft hydraulic systems.
Viewing 1 to 30 of 3396

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