Name | Support | Language | Availability | Edition date | Price | ||
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PDF |
English |
Active |
2/14/2022 |
€54.00 |
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Details
These formulae shall be used to determine drop dimensions for simple bend tube fittings utilizing flare and flareless end connection designs from 0° to 90° used in aircraft and aerospace applications. Individual design standards shall specify parameters, such as centerline bend radius (R), straight tangent length to accommodate bending equipment (X1 and X2), and nut to be used.
Additional Info
Author | Society of Automotive Engineers International (SAE) |
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Committee | G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies |
Published by | SAE |
Document type | Standard |
ICS | 49.080 : Aerospace fluid systems and components
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Number of pages | 4 |
Replace | SAE ARP 1676:2013-01-02 |
Document history | SAE ARP 1676:2013-01-02 |
Keyword | SAE 1676,SAE ARP1676A,SAE ARP1676A,SAE ARP 1676 |