Part Details | PIN-RIVET
5320-01-521-0442 A metallic or nonmetallic item, headed at one end, with a cylindrically shaped shank which may be tapered, grooved, or threaded. A locking collar or sleeve may be provided to perform the same holding action as the clinching portion of a conventional rivet. The shank may include an external wrenching facility which breaks off at a predetermined applied torque.
Alternate Parts: HLT1465312, HLT146-5-3-12, 3M91708312, 3M917-08-3-12, FIT798708312, FIT7987-08-3-12, HLT1465312, HLT146-5-3-12, HLT1465312, HLT146-5-3-12, HLT1465312, HLT146-5-3-12, HLT1465312, HLT146-5-3-12, HLT1465312, HLT146-5-3-12, 5320-01-521-0442, 01-521-0442, 5320015210442, 015210442
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JUN 08, 2004 | 01-521-0442 | 67165 ( PIN-RIVET ) |
REFERENCE DRAWINGS & PICTURES
STRAIGHT PAN
PIN-RIVET, STRAIGHT, THREADED
Cross Reference | NSN 5320-01-521-0442
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HLT146-5-3-12 | 92215 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 3M917-08-3-12 | 76301 | BOEING COMPANY, THEDBA BOEING |
| FIT7987-08-3-12 | 58998 | FASTENER INNOVATION TECHNOLOGY, INC.DBA F I T |
| HLT146-5-3-12 | 73197 | HI-SHEAR CORPORATION |
| HLT146-5-3-12 | 17446 | HUCK INTERNATIONAL, INC.DBA ARCONIC FASTENING SYSTEMS AND |
| HLT146-5-3-12 | L4528 | LISI AEROSPACE CANADA CORPDIV HI SHEAR HOLDINGS INC |
| HLT146-5-3-12 | 56878 | SPS TECHNOLOGIES, LLCDBA AEROSPACE DIVISION |
| HLT146-5-3-12 | 06725 | SPS TECHNOLOGIES, LLCDBA AIR INDUSTRIES |
Technical Data | NSN 5320-01-521-0442
| Characteristic | Specifications |
|---|---|
| MINIMUM TENSILE STRENGTH | 160000 POUNDS PER SQUARE INCH |
| HEAD STYLE | STRAIGHT PAN |
| HEAD HEIGHT | 0.055 INCHES MINIMUM AND 0.065 INCHES MAXIMUM |
| HEAD MAJOR DIAMETER | 0.306 INCHES MINIMUM AND 0.322 INCHES MAXIMUM |
| SHANK STYLE | PIN-RIVET, STRAIGHT, THREADED |
| FASTENER LENGTH | 0.187 INCHES NOMINAL |
| WIDTH BETWEEN FLATS | 0.079 INCHES MINIMUM AND 0.080 INCHES MAXIMUM |
| SHANK DIAMETER | 0.157 INCHES MINIMUM AND 0.159 INCHES MAXIMUM |
| GRIP LENGTH | 1.125 INCHES NOMINAL |
| LUBRICATION | CETYL ALCOHOL |
| SPECIAL FEATURES | 0.312 INCH THREAD ON STUD END; HEAD PROTRUDES 0.187 INCHES ON PIN GRIP END |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F/A-18 E/F AIRCRAFT |