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		                        | National Stock Number:
 5307-01-469-1477
 
 Federal Supply Class:
 5307
 
 National Item Identification Number:
 014691477
 
 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:
 
 | 11807-08-3-9 | 59563 | REID PRODUCTS INC. |  | 3M917-08-3-9 | 76301 | THE BOEING COMPANY |  | HL146-5-3-9 | 06725 | SPS TECHNOLOGIES, LLC |  | HL146-5-3-9 | 17446 | HUCK INTERNATIONAL, INC |  | HL146-5-3-9 | 56878 | SPS TECHNOLOGIES, LLC |  | FIT7987-08-3-9 | 58998 | FASTENER INNOVATION TECHNOLOGY, INC. |  | HL146-5-3-9 | 73197 | HI-SHEAR CORPORATION |  | HL146-5-3-9 | 92215 | HOWMET GLOBAL FASTENING SYSTEMS INC |  | HL146-5-3-9 | 97928 | HUCK INTL INC |  | HL146-5-3-9 | L4528 | LISI AEROSPACE CANADA CORP DIV HI SHEAR HOLDINGS INC | 
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 Techincal Specification:
 
 | MATERIAL | TITANIUM ALLOY UNS R54520 |  | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4928 ASSN STD 1ST MATERIAL RESPONSE OR |  |  | AMS 4967 ASSN STD 2ND MATERIAL RESPONSE |  | STYLE DESIGNATOR | SHOULDERED |  | SHOULDER DIAMETER | 0.306 INCHES MINIMUM AND |  |  | 0.322 INCHES MAXIMUM |  | SHOULDER LENGTH | 0.055 INCHES MINIMUM AND |  |  | 0.065 INCHES MAXIMUM |  | OVERALL LENGTH | 1.403 INCHES MINIMUM AND |  |  | 1.465 INCHES MAXIMUM |  | THREAD SERIES DESIGNATOR | UNJC NUT THREAD |  |  | UNJC STUD THREAD |  | NOMINAL THREAD SIZE | 0.164 INCHES NUT THREAD |  |  | 0.164 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 | 0.312 INCHES NOMINAL NUT THREAD |  |  | 0.312 INCHES NOMINAL STUD THREAD |  | SPECIAL FEATURES | LUBRICANT CETYL ALCHOL |  | CRITICALITY CODE JUSTIFICATION | AGAV |  | PART NAME ASSIGNED BY CONTROLLING AGENCY | PIN-RIVET,THREADED-SHEAR,PROTRUDING HEAD,HEX POINT DRIVE,TITANIUM ALLOY | 
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