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National Stock Number:
5307-01-521-3212
Federal Supply Class:
5307
National Item Identification Number:
015213212
Description:
STUD,SHOULDERED
Detail:
A HEADLESS FASTENER NOT EXCEEDING 12 INCHES (304.8 MM) IN LENGTH, THREADED EXTERNALLY ON BOTH ENDS WITH THREADS OF THE SAME NOMINAL DIAMETER. ALL OR PART OF THE UNTHREADED SECTION HAS A CROSS-SECTIONAL DIAMETER GREATER THAN THE NOMINAL STUD SIZE PLUS 0.020 INCHES (0.508 MM). IT MAY BE THREAD RELIEVED. SEE ALSO STUD, LOCKED IN.
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Manufacturer Information:
| 3M917-3-3-18 | 76301 | THE BOEING COMPANY | | AIC-L-146-3-3-18 | 06725 | SPS TECHNOLOGIES, LLC | | HL146-6-3-18 | 06725 | SPS TECHNOLOGIES, LLC | | HL146-6-3-18 | 17446 | HUCK INTERNATIONAL, INC | | HL146-6-3-18 | 56878 | SPS TECHNOLOGIES, LLC | | HL146-6-3-18 | 73197 | HI-SHEAR CORPORATION | | HL146-6-3-18 | 92215 | HOWMET GLOBAL FASTENING SYSTEMS INC | | HL146-6-3-18 | L4528 | LISI AEROSPACE CANADA CORP DIV HI SHEAR HOLDINGS INC |
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Techincal Specification:
| MATERIAL | TITANIUM ALLOY | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4928 ASSN STD SINGLE MATERIAL RESPONSE | | STYLE DESIGNATOR | SHOULDERED | | SHOULDER DIAMETER | 0.357 INCHES MINIMUM AND | | 0.377 INCHES MAXIMUM | | SHOULDER LENGTH | 0.064 INCHES MINIMUM AND | | 0.074 INCHES MAXIMUM | | NUT END SHANK LENGTH | 0.1825 INCHES MINIMUM AND | | 0.1925 INCHES MAXIMUM | | STUD END SHANK LENGTH | 1.120 INCHES MINIMUM AND | | 1.130 INCHES MAXIMUM | | STUD END SHANK DIAMETER | 0.1810 INCHES MINIMUM AND | | 0.1840 INCHES MAXIMUM | | NUT END SHANK DIAMETER | 0.1885 INCHES MINIMUM AND | | 0.1895 INCHES MAXIMUM | | OVERALL LENGTH | 1.9695 INCHES NOMINAL | | THREAD SERIES DESIGNATOR | UNJF NUT THREAD | | UNJF STUD THREAD | | NOMINAL THREAD SIZE | 0.190 INCHES NUT THREAD | | 0.190 INCHES STUD THREAD | | THREAD CLASS | 3A NUT THREAD | | 3A STUD THREAD | | THREAD QUANTITY PER INCH | 32 NUT THREAD | | 32 STUD THREAD | | THREAD DIRECTION | RIGHT-HAND NUT THREAD | | RIGHT-HAND STUD THREAD | | THREAD LENGTH | 0.325 INCHES NOMINAL NUT THREAD | | 0.325 INCHES NOMINAL STUD THREAD | | CRITICALITY CODE JUSTIFICATION | AGAV |
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