Part Details | PANEL SCREW ASSEMBLY
5305-01-068-1307 A headed, threaded fastening device over which may be assembled; (1) a stand-off; (2) a flanged bushing with washer(s) and/or a shouldered bushing without a flange, or it may have an internally threaded sleeve that is an integral part of the screw; a washer and an externally thread self-locking bushing that is driven by an inserted driver. Attached to panel by threaded bushing or by flaring end of stand-off, or bushing. Used in conjunction with a speed nut, nut plate, or driven into a threaded hole in the item that the panel is fastened to. May be spring loaded.
Alternate Parts: CA28080088P, CA28080-08-8P, CA28488P, CA2848-8P, CA28080088P, CA28080-08-8P, 5165623, HW100214001, HW1-00214-001, 5165623, 5305-01-068-1307, 01-068-1307, 5305010681307, 010681307
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | NOV 16, 1978 | 01-068-1307 | 33044 ( SCREW ASSEMBLY, PANEL ) |
REFERENCE DRAWINGS & PICTURES
CROWNED HEXAGON
Cross Reference | NSN 5305-01-068-1307
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CA28080-08-8P | D0680 | ALCOA FASTENING SYSTEMSFAIRCHILDFASTENERS EUROPE - CAMLOC |
| CA2848-8P | 29372 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| CA28080-08-8P | 29372 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 5165623 | 76301 | BOEING COMPANY, THEDBA BOEING |
| HW1-00214-001 | 66449 | MICROSOURCE, INC. |
| 5165623 | 53711 | NAVAL SEA SYSTEMS COMMAND |
Technical Data | NSN 5305-01-068-1307
| Characteristic | Specifications |
|---|---|
| THREAD SERIES DESIGNATOR | UNC |
| NOMINAL THREAD DIAMETER | 0.164 INCHES |
| THREAD QUANTITY PER INCH | 32 |
| THREAD CLASS | 2A |
| THREAD DIRECTION | RIGHT-HAND |
| THREAD LENGTH | 0.312 INCHES NOMINAL |
| FASTENER LENGTH | 0.500 INCHES NOMINAL |
| HEAD STYLE | 4 CROWNED HEXAGON |
| HEAD DIAMETER | 0.297 INCHES NOMINAL |
| MATERIAL ACCOMMODATED THICKNESS | 0.188 INCHES NOMINAL |
