NSN 5340-00-700-1621
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-00-700-1621 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: S616521012, S6165-21012, S616521012000, S6165-21012-000, S616521012, S6165-21012, 5340-00-700-1621, 00-700-1621, 5340007001621, 007001621
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-700-1621 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
SEAT
Cross Reference | NSN 5340-00-700-1621
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| S6165-21012 | D1081 | AIRBUS DEUTSCHLAND GMBH -WERKBREMEN- |
| S6165-21012-000 | 78286 | SIKORSKY AIRCRAFT CORPORATIONDBA SIKORSKY |
| S6165-21012 | 78286 | SIKORSKY AIRCRAFT CORPORATIONDBA SIKORSKY |
Technical Data | NSN 5340-00-700-1621
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL COMP 410 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-S-763, CLASS 410 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL HARDNESS RATING | RCB39.0 ROCKWELL C MAXIMUM AND 43.0 ROCKWELL C MAXIMUM |
| SURFACE TREATMENT | PASSIVATE |
| STYLE DESIGNATOR | SEAT |
| FEATURES PROVIDED | CASEHARDENED |