Part Details | BLIND RIVET
5320-00-005-6256 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: BACR15DR34, BACR15DR3-4, AF517134, AF5171-3-4, 1322OE52134, 1322OE5213-4, FON263943C4, FON2-6394-3C4, CCR264SS34, CCR264SS-3-4, CCR264SS34, CCR264SS-3-4, BACR15DR34, BACR15DR3-4, GR501AC34, GR501AC3-4, RV571A34, RV571A3-4, CCR264SS34, CCR264SS-3-4, BACR15DR34, BACR15DR3-4, CCR264SS34, CCR264SS-3-4, BACR15DR34, BACR15DR3-4, BACR15DR34, BACR15DR3-4, 114506884, 11450688-4, 5320-00-005-6256, 00-005-6256, 5320000056256, 000056256
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JUN 09, 1972 | 00-005-6256 | 00864 ( RIVET, BLIND ) |
REFERENCE DRAWINGS & PICTURES
FLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE - LESS THAN 135 DEG W OR W/O CHAMFER)
PULL THROUGH HOLLOW SHANK
Cross Reference | NSN 5320-00-005-6256
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| BACR15DR3-4 | 53551 | ALLFAST FASTENING SYSTEMS, LLC |
| AF5171-3-4 | 53551 | ALLFAST FASTENING SYSTEMS, LLC |
| 1322OE5213-4 | 97403 | CECOM LR CENTER |
| FON2-6394-3C4 | H1822 | FOKKER AEROSTRUCTURES B.V.DBA FOKKER AEROSTRUCTURES |
| CCR264SS-3-4 | F7652 | KLX AEROSPACE SOLUTIONS II SAS |
| CCR264SS-3-4 | FB009 | KLX INC |
| BACR15DR3-4 | 2N935 | M & M AEROSPACE HARDWARE, INC.DBA KLX AEROSPACE SOLUTIONS |
| GR501AC3-4 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| RV571A3-4 | 98996 | OLYMPIC FASTENING SYSTEMS INC |
| CCR264SS-3-4 | R1120 | SATAIR A/S |
| BACR15DR3-4 | 11815 | SPS TECHNOLOGIES, LLCDBA CHERRY AEROSPACE DIV |
| CCR264SS-3-4 | 11815 | SPS TECHNOLOGIES, LLCDBA CHERRY AEROSPACE DIV |
| BACR15DR3-4 | 81205 | THE BOEING COMPANYDBA BOEING |
| BACR15DR3-4 | 77272 | THE BOEING COMPANYDBA BOEING |
| 11450688-4 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5320-00-005-6256
| Characteristic | Specifications |
|---|---|
| HEAD STYLE | FLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE - LESS THAN 135 DEG W OR W/O CHAMFER) |
| SHANK STYLE | PULL THROUGH HOLLOW SHANK |
| HEAD MAJOR DIAMETER | 0.090 INCHES MAXIMUM |
| COUNTERSINK ANGLE | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
| FASTENER LENGTH | 0.328 INCHES NOMINAL |
| SHANK DIAMETER | 0.094 INCHES NOMINAL |
| GRIP LENGTH | 0.188 INCHES MINIMUM AND 0.250 INCHES MAXIMUM |
| EXPANSION DEVICE | SERRATED STEM-TYPE W |
| END ITEM IDENTIFICATION | W/S: TICONDEROGA CLASS CG (47); SPRUANCE CLASS DD (963); HELICOPTER, HH-53H PACE LOW; ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); HELICOPTER, ADVANCE ATTACK, AH-1W; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130); ENGINE, AIRCRAFT, TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, TF33-PW-102 (C-135E, EC-135H/K/P); HH-60L MEDIVAC |