NSN 5340-01-351-5758
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-01-351-5758 A circular item, usually having a flat or grooved flange, boss(es), and/or counterbore designed to accommodate the end of the spring. It is used to position the spring, but does not encase the spring or restrain lateral motion. It may be used in conjunction with a RETAINER, HELICAL COMPRESSION SPRING. Excludes WASHER (1), (as modified); SEAT, BALL SOCKET and HOLDER, SPRING. See also ROTOR, ENGINE POPPET VALVE.
Alternate Parts: 184226001, 184226-001, 184226001, 184226-001, 184226001, 184226-001, 5340-01-351-5758, 01-351-5758, 5340013515758, 013515758
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 10, 1992 | 01-351-5758 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5340-01-351-5758
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 184226-001 | 0UES3 | MOOG INC. |
| 184226-001 | 94697 | MOOG INC.DBA MOOG |
| 184226-001 | 19156 | MOOG INC.DIV MOOG AIRCRAFT, SALT LAKE |
Technical Data | NSN 5340-01-351-5758
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL COMP XM-12 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5659 ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL HARDNESS RATING | RCB35.0 ROCKWELL C MAXIMUM AND 42.0 ROCKWELL C MAXIMUM |
| SURFACE TREATMENT | PASSIVATE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-35 FED SPEC SINGLE TREATMENT RESPONSE |
| OVERALL HEIGHT | 0.0920 INCHES MINIMUM AND 0.1020 INCHES MAXIMUM |
| END DIAMETER | 1.6000 INCHES NOMINAL |
| BORE DIAMETER | 1.2050 INCHES MINIMUM AND 1.2100 INCHES MAXIMUM |
| COUNTERSINK ANGLE IN DEG | 45.0 |
| DESIGN TYPE | SOLID |