NSN 5325-01-530-2468
Part Details | PANEL FASTENER INSERT
5325-01-530-2468 An insert which must have a hole that may be internally threaded with a flange on one end. It may have an undercut on the end opposite the flange to provide a shoulder to allow for mating with another insert. Pre-assembled items will consist of an expansion sleeve and a body which may be flared. Internally threaded items may have a self-locking feature. Excludes INSERT, SCREW THREAD.
Alternate Parts: CA3580366, CA358036-6, 501166, 50-116-6, CA3580366, CA358036-6, 1230046, 123004-6, 5325-01-530-2468, 01-530-2468, 5325015302468, 015302468
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | MAY 19, 2005 | 01-530-2468 | 37444 ( INSERT, PANEL FASTENER ) |
REFERENCE DRAWINGS & PICTURES
PROTRUDING FLANGE
Cross Reference | NSN 5325-01-530-2468
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CA358036-6 | 29372 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 50-116-6 | 97499 | BELL HELICOPTER TEXTRON INC.DBA BELL HELICOPTER |
| CA358036-6 | 97499 | BELL HELICOPTER TEXTRON INC.DBA BELL HELICOPTER |
| 123004-6 | 60119 | MONADNOCK COMPANY, THEDBA LISI AEROSPACE |
Technical Data | NSN 5325-01-530-2468
| Characteristic | Specifications |
|---|---|
| INSERT STYLE | PROTRUDING FLANGE |
| FLANGE DIAMETER | 0.485 INCHES MINIMUM AND 0.495 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.008 INCHES MINIMUM AND 0.012 INCHES MAXIMUM |
| BODY DIAMETER | 0.257 INCHES MINIMUM AND 0.261 INCHES MAXIMUM |
| HOLE TYPE | PLAIN |
| HOLE DIAMETER | 0.237 INCHES MINIMUM AND 0.240 INCHES MAXIMUM |
| SPECIAL FEATURES | LENGTH .305 TO .315 INCHES; GRP RANGE .211 TO .240;ESSENTIAL TO WEAPON SYSTEM PERFORMANCE OR OPERATION, OR THE PRESERVATION OF LIFE OR SAFETY OF OPERATING PERSONNEL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | FAIRING INSTL; PANEL INSTL; V-22 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | GROMMET,METALLIC |