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Viewing 1 to 30 of 3498
2017-12-13
WIP Standard
AS6075A
Scope unavailable.
2017-12-13
WIP Standard
AS6105A
Scope unavailable.
2017-12-13
WIP Standard
AS6213A
Scope is unavailable.
2017-12-13
WIP Standard
AS6099A
Scope unavailable.
2017-12-13
WIP Standard
AS6103A
Scope unavailable.
2017-12-13
WIP Standard
AS6104A
Scope is unavailable.
CURRENT
2017-12-12
Standard
AS6369/2
This is the sheet metal flange design standard for the new AS6369 specification.
CURRENT
2017-12-12
Standard
AS6369
This SAE Aerospace Standard (AS) establishes the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft pneumatic systems. The coupling joint assembly, hereafter referred to as "the joint", shall operate within the temperature range of -65 °F external ambient to +800 °F internal fluid.
CURRENT
2017-12-12
Standard
AS6369/1
SCOPE IS UNAVAILABLE.
CURRENT
2017-12-12
Standard
AS6369/3
This is the solid flange design standard for the new AS6369 specification.
2017-12-08
WIP Standard
AS85421B
Revision clarifies qualification/manufacturing details regarding initial form of fitting (standard near-net forgings, oversize forgings or bar stock). Additionally, replacing the lot-to-lot destructive testing with standardized periodic test procedures.
CURRENT
2017-12-07
Standard
AS1650E
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. AS1650 was not designed for the new certification requirements for flammable leakage zones and fuel tanks for lightning protection and assembly redundancy. As such their use and installation may require additional efforts and equipment to support new FAA CFR compliance. The AS7510 flexible coupling should be the preferred coupling for use in flammable leakage zones and fuel tanks that require service life and functionality for lightning protection and part redundancy.
CURRENT
2017-11-21
Standard
AS4227C
Scope is unavailable.
CURRENT
2017-11-21
Standard
AS6495B
SCOPE IS UNAVAILABLE.
CURRENT
2017-11-20
Standard
AS931C
SCOPE IS UNAVAILABLE.
CURRENT
2017-11-13
Standard
AS5420G
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems with an environmental operating temperature range of -65 °F (-54 °C) to +160 °F (+71 °C).
2017-11-13
WIP Standard
AS1895/7F
SCOPE IS UNAVAILABLE.
CURRENT
2017-11-03
Standard
AS85421/10D
SCOPE IS UNAVAILABLE.
CURRENT
2017-10-26
Standard
AS101A
NO SCOPE AVAILABLE
CURRENT
2017-10-25
Standard
AS1002J
NO SCOPE AVAILABLE.
2017-10-20
WIP Standard
AS4108C
This specification defines the requirements for A286 cres T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings at 1000 °F maximum ambient temperature.
2017-10-20
WIP Standard
AS1895E
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.
Viewing 1 to 30 of 3498

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