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Fitting Assembly - 24° Cone Flareless per AS5827, 5080 psi, Port Connection, Port Preparation, Installation and Removal of AS5550 and AS5865
- Aerospace Standard
Published March 23, 2017 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Standard (AS) establishes the requirements for port preparation, installation, and removal procedure for AS5550 fitting assembly and AS5865 fitting reducer assembly, and is applicable when specified on engineering drawings, or in procurement documents.
Port preparation tooling consolidated into Table 3C. Addition of alternate tooling numbers in Tables 1B, 2B, and 3C. Correct Table 2A, Port Number 24 Installation Torque to 1900 through 2100 lbf.in. Add user definition requirement if torque values desired are other than those listed in Tables 1A or 2A. Update Section 5 to improve port cavity definition. Update 6.2.4 and 7.2.4 to recognize use of the sealants/primers and discourage use of Zinc Chromate primer. Update 6.2.5 and 7.2.5 for installation torque limits. Correction of references.
|Aerospace Standard||Test Methods for Tube-Fitting Assemblies|
|Aerospace Standard||FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI|
|Aerospace Standard||Adapters - Port Connection, Ring Locked Design, Installation and Removal of|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Table 1A||O-ring, stand-off and torque for AS5550|
|Table 1B||Tooling - installation and removal for AS5550|
|Table 2A||O-ring, stand-off and torque, port preparation tooling for AS5865|
|Table 2B||Tooling continued - installation and removal for AS5865|
|Table 3A||Threads and dimensions A-E|
|Table 3B||Dimensions F-N|
|Table 3C||Port preparation tooling and serrations gage|
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