This content is not included in your SAE MOBILUS subscription, or you are not logged in.
COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING
- Aerospace Standard
Published March 01, 1998 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document 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, is designed for use from -65 to 400 °F and at 125 psi operating pressure.
|Aerospace Standard||Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Metric|
|Aerospace Standard||Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement Specification|
|Aerospace Material Specification||Paste Adhesive for Core Restoration Part 1 - General Requirements|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|TABLE 1||Physical Requirements|
|TABLE 2||Tube Size and Wall Thickness|
|TABLE 3||Test Schedule and Sequence|
|TABLE 4||Vibration Levels (Sinusoidal)|
|TABLE 5||Vibration Test Times|
|TABLE 6||Vibration Levels (Nongunfire)|
|TABLE 7||Acceleration Levels (Nongunfire)|
|TABLE 8||Vibration Levels (Gunfire)|
|TABLE 9||Vibration Test Times (Gunfire)|
|TABLE 11||Defect Characteristics|
|TABLE 12||Classification of Defects|
|TABLE 13||CLAMP BLOCK DIM’S. MATERIAL: ALUMINUM ALLOY|
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This Committee is responsible for developing and maintaining standards for design, test, and procurement of fluid systems part standards to improve reliability and economy. Their primary focus is on AS standards development and support of military standards. The Committee also develops ISO standards in a Subcommittee Advisory Group (SCAG) to ISO/TC 20/SC 10, and SAE-MA derivatives thereof.Structure: SAE G-3 -- Parent committee SAE G-3A -- Aerospace Couplings Subcommittee SAE G-3B -- Aerospace Fittings Subcommittee SAE G-3D -- Aerospace Hose Subcommittee SAE G-3E - Aerospace Tubing Assemblies Subcommittee U.S. SCAG to ISO/TC 20/SC 10 -- ISO standards Major projects: Support of Military Standards Reform Support of military standard conversions to MIL-PERF and MIL-DTL. Development of AS replacements for military standards designated for conversion. Establish document to list G-3 accepted replacements for replaced part standards and military back-up specifications. Development of PRI QML/QPL Development of Performance Review Institute (PRI) process for approval and surveillance of manufacturers (Qualified Manufacturer List, QML) and for approval of standard parts as qualified for use (Qualified Parts List, QPL). Development of ISO Standards, Imperial Units ISO/TC 20/SC 10 standards have typically been developed in SI units. The ISO has approved development of inch-based ISO standards to support commercial aviation. Basic design, test, and procurement specifications will be selected from military standards that are to be converted to Non-Government standard (NGS) and developed as ISO standards.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.