NSN 5340-00-931-5114
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-00-931-5114 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: 2633300, 5340-00-931-5114, 00-931-5114, 5340009315114, 009315114
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | SEP 16, 1966 | 00-931-5114 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
SEAT
Cross Reference | NSN 5340-00-931-5114
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2633300 | 06848 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 5340-00-931-5114
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | SEAT |
| OVERALL HEIGHT | 0.0430 INCHES NOMINAL |
| END DIAMETER | 0.4300 INCHES NOMINAL |
| DISTANCE FROM END TO FIRST STEP | 0.2200 INCHES NOMINAL |
| FIRST STEP DIAMETER | 1.0600 INCHES NOMINAL |
| BORE DIAMETER | 0.8100 INCHES NOMINAL |
| COUNTERBORE DIAMETER | 0.9500 INCHES NOMINAL |
| BORE TAPER IN DEG | 30.0 |
| SPHERICAL SEAT TOP RADIUS | 0.0100 INCHES NOMINAL |
| FSC APPLICATION DATA | AIRCRAFT ENGINE FUEL CONTROL |