NSN 5340-01-125-8239
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-01-125-8239 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: 74A6705012001, 74A670501-2001, 5340-01-125-8239, 01-125-8239, 5340011258239, 011258239
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | FEB 01, 1982 | 01-125-8239 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
SEAT
Cross Reference | NSN 5340-01-125-8239
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 74A670501-2001 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 5340-01-125-8239
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225 TO 9, ALLOY 7075, T7351 FED SPEC SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | SEAT |
| OVERALL HEIGHT | 0.1200 INCHES NOMINAL |
| END DIAMETER | 0.4380 INCHES NOMINAL |
| DISTANCE FROM END TO FIRST STEP | 0.0700 INCHES NOMINAL |
| FIRST STEP DIAMETER | 0.6700 INCHES NOMINAL |
| BORE DIAMETER | 0.2500 INCHES NOMINAL |
| SPHERICAL SEAT TOP RADIUS | 0.0600 INCHES NOMINAL |
| DESIGN TYPE | SOLID |
| SPECIAL FEATURES | NOT CASEHARDENED |
| FSC APPLICATION DATA | INTERLOCK,AILERON WING FOLD SYSTEM |