NSN 5325-00-726-6699
Part Details | TURNLOCK FASTENER STUD ASSEMBLY
5325-00-726-6699 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: 26S83, 26S8-3, 26S83, 26S8-3, 26S803, 26S8-03, 3D00633AC, 3D0063-3AC, HK26BC3, HK26BC-3, HS44313, HS4431-3, 11260043, 1126004-3, 95032678, 950326-78, 721632203, 721632-203, HE12800283103, HE128-0028-3103, BACS21Y3R, BACS21EE3R, 250015, 25001-5, 5325-00-726-6699, 00-726-6699, 5325007266699, 007266699
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-726-6699 | 18484 ( STUD ASSEMBLY, TURNLOCK FASTENER ) |
REFERENCE DRAWINGS & PICTURES
FLAT FILLISTER
STUD ASSEMBLY
Cross Reference | NSN 5325-00-726-6699
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 26S8-3 | D0680 | ALCOA FASTENING SYSTEMSFAIRCHILDFASTENERS EUROPE - CAMLOC |
| 26S8-3 | 71286 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 26S8-03 | 71286 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 3D0063-3AC | 88277 | BOEING COMPANY, THEDBA BOEING |
| HK26BC-3 | 69370 | HO-HO-KUS, INC. |
| HS4431-3 | 02731 | MCDONNELL DOUGLAS HELICOPTER CO INC |
| 1126004-3 | 60119 | MONADNOCK COMPANY, THEDBA LISI AEROSPACE |
| 950326-78 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| 721632-203 | 82577 | RAYTHEON COMPANYDBA RAYTHEON |
| HE128-0028-3103 | 89372 | ROCKWELL INTERNATIONAL CORPNORTH AMERICAN AIRCRAFT OPNS |
| BACS21Y3R | 77272 | THE BOEING COMPANYDBA BOEING |
| BACS21EE3R | 81205 | THE BOEING COMPANYDBA BOEING |
| 25001-5 | 51998 | UNIVERSAL PROPULSION COMPANY INCDBA GOODRICH DIV UNIVERSAL |
Technical Data | NSN 5325-00-726-6699
| Characteristic | Specifications |
|---|---|
| TURNLOCK STUD HEAD STYLE | FLAT FILLISTER |
| DIAMETER | 0.303 INCHES NOMINAL |
| STUD HEAD HEIGHT | 0.093 INCHES NOMINAL |
| STUD ASSEMBLY STYLE | STUD ASSEMBLY |
| DISTANCE FROM ENGAGING MEMBER TO LARGEST BEARING SURFACE OF HEAD | 0.602 INCHES MINIMUM AND 0.617 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 | 0.060 INCHES MINIMUM AND 0.119 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | W/S:TACTICAL AIR OPNS MODULE (AN/TYQ-(23); AIRCRAFT, C-18A, EC-18B; AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); AIRCRAFT, C-2A (REPROCURED); AIRCRAFT, AIRLIFTER C-17A; HELICOPTER, SEARCH AND RESCUE, HH-60H; HELICOPTER, HH-53H PAVE LOW; HELICOPTER, MH-53E; HELICOPTER, CARRIER BASED ASW, SH-60F |
