Part Details | TURNLOCK FASTENER STUD ASSEMBLY
5325-00-797-3002 A STUD, TURNLOCK FASTENER over which may be assembled an EYELET, TURNLOCK FASTENER. Stud(s) without cam slots or cam lead threads are provided with a crosspin or eared nut for locking with the mating RECEPTACLE, TURNLOCK FASTENER. May be spring loaded. For like items having a threaded fastener, see SCREW ASSEMBLY, PANEL or SCREW, PANEL FASTENER.
Alternate Parts: 26S81, 26S8-1, 26S81AC, 26S8-1AC, 26S81, 26S8-1, 3D00631AC, 3D0063-1AC, HK26BC1, HK26BC-1, 11260041, 1126004-1, BACS21Y1R, 10331395, 10331375, 5325-00-797-3002, 00-797-3002, 5325007973002, 007973002
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1962 | 00-797-3002 | 18484 ( STUD ASSEMBLY, TURNLOCK FASTENER ) |
REFERENCE DRAWINGS & PICTURES
FLAT FILLISTER
STUD ASSEMBLY
Cross Reference | NSN 5325-00-797-3002
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 26S8-1 | D0680 | ALCOA FASTENING SYSTEMSFAIRCHILDFASTENERS EUROPE - CAMLOC |
| 26S8-1AC | 71286 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 26S8-1 | 71286 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 3D0063-1AC | 88277 | BOEING COMPANY, THEDBA BOEING |
| HK26BC-1 | 69370 | HO-HO-KUS, INC. |
| 1126004-1 | 60119 | MONADNOCK COMPANY, THEDBA LISI AEROSPACE |
| BACS21Y1R | 81205 | THE BOEING COMPANYDBA BOEING |
| 10331395 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 10331375 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5325-00-797-3002
| Characteristic | Specifications |
|---|---|
| TURNLOCK STUD HEAD STYLE | FLAT FILLISTER |
| DIAMETER | 0.251 INCHES MINIMUM AND 0.256 INCHES MAXIMUM |
| STUD HEAD HEIGHT | 0.069 INCHES MINIMUM AND 0.076 INCHES MAXIMUM |
| STUD ASSEMBLY STYLE | STUD ASSEMBLY |
| DISTANCE FROM ENGAGING MEMBER TO LARGEST BEARING SURFACE OF HEAD | 0.542 INCHES MINIMUM AND 0.557 INCHES MAXIMUM |
| EYELET OUTSIDE DIAMETER | 0.244 INCHES MINIMUM AND 0.250 INCHES MAXIMUM |
| EYELET LENGTH | 0.322 INCHES NOMINAL |
| DRIVE TYPE | CROSS RECESS |
| MATERIAL ACCOMMODATED THICKNESS | 0.030 INCHES MINIMUM AND 0.419 INCHES MAXIMUM |