NSN 5325-00-682-1447
Part Details | TURNLOCK FASTENER STUD ASSEMBLY
5325-00-682-1447 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: 260010SW, 2600-10SW, HS443110SW, HS4431-10SW, 26HV10, G24334810, G243348-10, HS443110SW, HS4431-10SW, 112601410, 1126014-10, 9081614, 1055979510, 10559795-10, 10559795, 5325-00-682-1447, 00-682-1447, 5325006821447, 006821447
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-682-1447 | 18484 ( STUD ASSEMBLY, TURNLOCK FASTENER ) |
REFERENCE DRAWINGS & PICTURES
FLAT COUNTERSUNK
STUD ASSEMBLY
Cross Reference | NSN 5325-00-682-1447
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2600-10SW | 71286 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| HS4431-10SW | 8V613 | BOEING COMPANY, THEDBA BOEING |
| 26HV10 | 69370 | HO-HO-KUS, INC. |
| G243348-10 | 01714 | LUCENT TECHNOLOGIES INCADVANCED TECHNOLOGY SYSTEMS |
| HS4431-10SW | 02731 | MCDONNELL DOUGLAS HELICOPTER CO INC |
| 1126014-10 | 60119 | MONADNOCK COMPANY, THEDBA LISI AEROSPACE |
| 9081614 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 10559795-10 | 19200 | US ARMY ARDEC RDECOM |
| 10559795 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5325-00-682-1447
| Characteristic | Specifications |
|---|---|
| TURNLOCK STUD HEAD STYLE | 0 FLAT COUNTERSUNK |
| HEAD LENGTH | 0.700 INCHES MINIMUM AND 0.740 INCHES MAXIMUM |
| STUD HEAD HEIGHT | 0.360 INCHES MINIMUM AND 0.400 INCHES MAXIMUM |
| STUD ASSEMBLY STYLE | STUD ASSEMBLY |
| DISTANCE FROM ENGAGING MEMBER TO LARGEST BEARING SURFACE OF HEAD | 0.812 INCHES MINIMUM AND 0.827 INCHES MAXIMUM |
| EYELET OUTSIDE DIAMETER | 0.244 INCHES MINIMUM AND 0.250 INCHES MAXIMUM |
| EYELET LENGTH | 0.322 INCHES NOMINAL |
| MATERIAL ACCOMMODATED THICKNESS | 0.300 INCHES MINIMUM AND 0.329 INCHES MAXIMUM |