Part Details | PANEL SCREW ASSEMBLY
5305-01-192-1431 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: 9130023D4, 913002-3-D-4, HSGB79003D4, HSGB7900-3-D-4, HSGB79003D4, HSGB7900-3-D-4, HSGB79003D4, HSGB7900-3-D-4, 9130023D4, 913002-3-D-4, 9130023D4, 913002-3-D-4, 5305-01-192-1431, 01-192-1431, 5305011921431, 011921431
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | OCT 17, 1984 | 01-192-1431 | 33044 ( SCREW ASSEMBLY, PANEL ) |
REFERENCE DRAWINGS & PICTURES
HEXAGON
HEXAGON
Cross Reference | NSN 5305-01-192-1431
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 913002-3-D-4 | 5R793 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| HSGB7900-3-D-4 | 17446 | HUCK INTERNATIONAL, INC.DBA ARCONIC FASTENING SYSTEMS AND |
| HSGB7900-3-D-4 | 0HDW7 | HUCK INTERNATIONAL, INC.DBA ARCONIC FASTENING SYSTEMS AND |
| HSGB7900-3-D-4 | 97928 | HUCK INTL INC |
| 913002-3-D-4 | 09205 | LOCKHEED MARTIN CORPELECTRONICS AND MISSILES DIV |
| 913002-3-D-4 | 04939 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
Technical Data | NSN 5305-01-192-1431
| Characteristic | Specifications |
|---|---|
| THREAD SERIES DESIGNATOR | UNJF |
| NOMINAL THREAD DIAMETER | 0.190 INCHES |
| THREAD QUANTITY PER INCH | 32 |
| THREAD CLASS | 3A |
| THREAD DIRECTION | RIGHT-HAND |
| THREAD LENGTH | 0.303 INCHES MINIMUM AND 0.313 INCHES MAXIMUM |
| FASTENER LENGTH | 0.990 INCHES NOMINAL |
| HEAD STYLE | HEXAGON |
| HEAD HEIGHT | 0.145 INCHES MINIMUM AND 0.150 INCHES MAXIMUM |
| WIDTH BETWEEN FLATS | 0.305 INCHES MINIMUM AND 0.312 INCHES MAXIMUM |
| INTERNAL DRIVE STYLE | HEXAGON |
| WIDTH ACROSS FLATS | 0.156 INCHES MINIMUM AND 0.158 INCHES MAXIMUM |
| MATERIAL ACCOMMODATED THICKNESS | 0.188 INCHES MINIMUM AND 0.250 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | F414 ENGINE(F/A-18F&GAIRCRAFT);AIRCRAFT;HORNETF/A-18 |