NSN 5325-00-621-3195
Part Details | RETAINING RING
5325-00-621-3195 A resilient metal item, circular or nearly circular, which is designed to be inserted into an internal or external groove and retained by its own spring action, or it may have external prongs or projections designed to be inserted into a hole and retained by spring action of the prongs which grip by imbedding into the material. For items having internal prongs which perform the same function, see PUSH ON NUT. It is used to keep and/or lock a part(s) in position, as a ball bearing on a shaft or in a housing. See also CLIP, RETAINING and PIN, LOCK. Excludes RING, CONNECTING, ROUND.
Alternate Parts: HS3014RR200, 3415200P, 3415-200P, 6260019150, 626-001-9150, HS3014RR200, M2742630149A, M274263149A, M27426-3149A, MILDTL27426, MIL-DTL-27426, 645121A200, HS3014RR200, WH200, WH-200, HS3014RR200, RR200, RR-200, 8528835, 8528834, RR200, 5325-00-621-3195, 00-621-3195, 5325006213195, 006213195
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-621-3195 | 07623 ( RING, RETAINING ) |
REFERENCE DRAWINGS & PICTURES
ROUND
SPIRAL
Cross Reference | NSN 5325-00-621-3195
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HS3014RR200 | 8V613 | BOEING COMPANY, THEDBA BOEING |
| 3415-200P | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 626-001-9150 | 70210 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| HS3014RR200 | 02731 | MCDONNELL DOUGLAS HELICOPTER CO INC |
| M2742630149A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M27426-3149A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-DTL-27426 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 645121A200 | 92003 | PARKER HANNIFIN CORPORATIONDIV AEROSPACE GROUP HEADQUARTERS |
| HS3014RR200 | 0FGC4 | SEY TEC, INC. |
| WH-200 | 51814 | SMALLEY STEEL RING CO. |
| HS3014RR200 | 51814 | SMALLEY STEEL RING CO. |
| RR-200 | 80756 | SPIROLOX, INC. |
| 8528835 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 8528834 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| RR200 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
Technical Data | NSN 5325-00-621-3195
| Characteristic | Specifications |
|---|---|
| STRENGTH RATING | 211000.0 POUNDS PER SQUARE INCH MINIMUM TENSILE |
| CASEHARDENING INDICATOR | NOT CASEHARDENED |
| RING STYLE | SPIRAL |
| CROSS-SECTIONAL SHAPE STYLE | 2 ROUND |
| USAGE DESIGN | INTERNAL |
| INSIDE DIAMETER | 1.835 INCHES MINIMUM AND 1.855 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 2.091 INCHES MINIMUM AND 2.111 INCHES MAXIMUM |
| MAJOR THICKNESS | 0.046 INCHES MINIMUM AND 0.052 INCHES MAXIMUM |