NSN 5342-01-448-9570
Part Details | WEAPON SYSTEM RESILIENT MOUNT
5342-01-448-9570 An item made of material having elastic properties. It may have rigid mounting facilities such as a flange(s), sleeve(s), stud(s) or the like. It is designed to isolate or dampen shock and/or vibration of a continuous or intermittent origin and serve as a support for a weapon system component to be isolated. Excludes MOUNT, RESILIENT, UTILITY; SPRING (as modified); BUMPER, NONMETALLIC; BUMPER, RUBBER; BUSHING, NONMETALLIC; hydraulic and pneumatic shock absorbers, dash-pots, grommets, and shock pads.
Alternate Parts: 9M8688, 9M868-8, 247654, 24765-4, 5342-01-448-9570, 01-448-9570, 5342014489570, 014489570
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | SEP 16, 1997 | 01-448-9570 | 53589 ( MOUNT, RESILIENT, WEAPON SYSTEM ) |
REFERENCE DRAWINGS & PICTURES
ROUND W/FLANGE THREADED STUD
Cross Reference | NSN 5342-01-448-9570
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9M868-8 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 24765-4 | 81860 | HUTCHINSON AEROSPACE & INDUSTRY,INC. |
Technical Data | NSN 5342-01-448-9570
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | ROUND W/FLANGE THREADED STUD |
| INSIDE DIAMETER | 0.285 INCHES NOMINAL |
| FLANGE THICKNESS | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
| DISTANCE BETWEEN MOUNTING HOLE CENTERS | 1.578 INCHES MINIMUM AND 1.598 INCHES MAXIMUM |
| FLANGE LENGTH | 2.161 INCHES MINIMUM AND 2.191 INCHES MAXIMUM |
| FLANGE WIDTH | 1.080 INCHES MINIMUM AND 1.150 INCHES MAXIMUM |
| DISTANCE FROM FLANGE TO END | 0.411 INCHES MINIMUM AND 0.491 INCHES MAXIMUM |
| FLANGE MOUNTING HOLE DIAMETER | 0.186 INCHES MINIMUM AND 0.206 INCHES MAXIMUM |
| LOAD/FREQUENCY RANGE | 8.0 LB LOAD FOR 21 TO 25 HERTZ |
| HEIGHT | 0.761 INCHES MINIMUM AND 0.801 INCHES MAXIMUM |
| MAXIMUM LOAD RATING | 8.0 POUNDS |
| SPECIAL FEATURES | REQUESTED NAME MOUNT, RESILIENT-LOW PROFILE, 2 LUG, SELF-LOCKING THREADED INSERT |
| END ITEM IDENTIFICATION | F15I |