Part Details | BLIND RIVET
5320-00-117-7341 An item consisting of two or more of the following components: stem, rivet body, sleeve, expander, bolt, and collar. It is a headed fastening device with the shank designed to be expanded by means of a separate or integral stem or mandrel, or bolt and expander. It is designed to be installed or expanded from one side only. Excludes NUT, BLIND ASSEMBLY.
Alternate Parts: 45946, 459-4-6, DR134A6, 39A37, MILR7885, MIL-R-7885, MS20602D46, MS20602D4-6, MS20602AD46, MS20602AD4-6, NAF11954A6, NAF1195-4A6, CVC13706, CVC1370-6, 5320-00-117-7341, 00-117-7341, 5320001177341, 001177341
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-117-7341 | 00864 ( RIVET, BLIND ) |
REFERENCE DRAWINGS & PICTURES
BELT
Cross Reference | NSN 5320-00-117-7341
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 459-4-6 | 80049 | DEPARTMENT OF THE AIR FORCE |
| DR134A6 | 18873 | DU PONT E I DE NEMOURS AND CO INCSECURITY DIRECTOR/LEGAL DEPT |
| 39A37 | 72914 | GRIMES AEROSPACE COMPANYDBA HONEYWELL |
| MIL-R-7885 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MS20602D4-6 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| MS20602AD4-6 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| NAF1195-4A6 | 80020 | NAVAL AIR WARFARE CENTER AIRCRAFTDIVISION CODE 4.8.8.0.0.B BLDG 148-2 |
| CVC1370-6 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 5320-00-117-7341
| Characteristic | Specifications |
|---|---|
| HEAD STYLE | 9 BELT |
| HEAD HEIGHT | 0.050 INCHES NOMINAL |
| HEAD MAJOR DIAMETER | 0.250 INCHES NOMINAL |
| FASTENER LENGTH | 0.170 INCHES NOMINAL |
| SHANK DIAMETER | 0.125 INCHES NOMINAL |
| GRIP LENGTH | 0.046 INCHES MINIMUM AND 0.065 INCHES MAXIMUM |
| SPECIFICATION/STANDARD DATA | 81349-MIL-R-7885 GOVERNMENT SPECIFICATION AND 96906-MS20602 TO CANCELED TO GOVERNMENT STANDARD |
| NONDEFINITIVE SPEC/STD DATA | 1 TYPE AND 1 CLASS AND A STYLE |