Refine Your Search

Date

Date

Topic

Topic

Medical, health, and wellness Hoses and tubes Materials G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Search Results

Viewing 1 to 20 of 3702
123Next >Last >>
Sort by published
Standard

Hose Assemblies, Installed, Visual Inspection Guide for
2024-02-27
CURRENT
ARP1658C
This SAE Aerospace Recommended Practice (ARP) covers visible surface defects on aerospace hose assemblies which have been installed and are functioning within a working environment at the time of visual inspection.
Standard

Fittings, Welded, Hydraulic, Titanium, Corrosion-Resistant Steel and Nickel, 3000 psi Hydraulic
2024-02-23
CURRENT
AS1576G
This document defines the requirements for weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3AL-2.5V titanium, 21Cr-6Ni-9Mn CRES, and 718 nickel alloy tubing. Fitting standards covered by this specification include non-separable welded elbow, tee, and reducer fittings, and reconnectable 24-degree cone fittings, such as sleeves and unions.
Standard

Coupling Assembly, V-Retainer, High Pressure High Temperature, Pneumatic Tube
2024-02-16
CURRENT
AS1895F
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.
Standard

Coupling Assembly, Threadless, Flexible, Self-Locking, Fixed Cavity, High Conductivity, Self-Bonding, Part Specification
2023-12-18
CURRENT
AS7510B
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive, self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system. FAR 23.954, FAR 25.603, FAR 25.605, FAR 25.609, FAR 25.613, FAR 25.901, FAR 25.954, and FAR 25.981 certification requirements have identified the need for high-current capable flexible fluid assembled couplings. The coupling assembly does not require inspection or maintenance to remain current capable for the life of the aircraft.
123Next >Last >>
X