Part Details | SHOULDERED STUD
5307-01-644-2341 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.
Alternate Parts: HL346641, HL346-6-4-1, HL346641, HL346-6-4-1, HL346641, HL346-6-4-1, HL346641, HL346-6-4-1, HL346641, HL346-6-4-1, 5307-01-644-2341, 01-644-2341, 5307016442341, 016442341
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | APR 27, 2015 | 01-644-2341 | 15946 ( STUD, SHOULDERED ) |
REFERENCE DRAWINGS & PICTURES
SHOULDERED
Cross Reference | NSN 5307-01-644-2341
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HL346-6-4-1 | 73197 | HI-SHEAR CORPORATION |
| HL346-6-4-1 | 17446 | HUCK INTERNATIONAL, INC.DBA ARCONIC FASTENING SYSTEMS AND |
| HL346-6-4-1 | 80539 | SPS TECHNOLOGIES, LLCDBA AEROSPACE FASTENERS GROUP |
| HL346-6-4-1 | 06725 | SPS TECHNOLOGIES, LLCDBA AIR INDUSTRIES |
| HL346-6-4-1 | 60516 | WEST COAST AEROSPACE INC |
Technical Data | NSN 5307-01-644-2341
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY UNS R56400 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 OR AMS4967 ASSN STD SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | SHOULDERED |
| SHOULDER DIAMETER | 0.370 INCHES MINIMUM AND 0.390 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.064 INCHES MINIMUM AND 0.074 INCHES MAXIMUM |
| NUT END SHANK LENGTH | 0.325 INCHES NOMINAL |
| STUD END SHANK LENGTH | 0.325 INCHES NOMINAL |
| STUD END SHANK DIAMETER | 0.1885 INCHES MINIMUM AND 0.1895 INCHES MAXIMUM |
| NUT END SHANK DIAMETER | 0.2172 INCHES MINIMUM AND 0.2182 INCHES MAXIMUM |
| OVERALL LENGTH | 1.026 INCHES MINIMUM |
| SPECIAL FEATURES | FINISH: CETYL ALCOHOL LUBE PER HI-SHEAR SPEC 305; THREADS MODIFIED - ROLLED PER MIL-S-8879; HAS INTERNAL HEX DRIVE, 0.0791-0.0806 ACROSS FLATS X 0.080-0.100 IN. DEEP; EXTERNAL THREADS ON DRIVE END ARE 0.250 IN LONG; EXTERNAL THREADS ON OTHER END ARE 0.063 IN. LONG; HEAT: 160,000 PSI TENSILE MINIMUM; DOUBLE SHEAR: 6,130 POUNDS MINIMUM; TENSION: 3,160 POUNDS MINIMUM |
| END ITEM IDENTIFICATION | FIGHTER AIRCRAFT (F18 E/F) |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | THREADED STUD PIN, PROTUDING HEAD, TITANIUM ALLOY |