NSN 5340-00-679-3288
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-00-679-3288 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: 75232, 75232, 75232, 75232, 5340-00-679-3288, 00-679-3288, 5340006793288, 006793288
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-679-3288 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5340-00-679-3288
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 75232 | 72599 | ALLIEDSIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| 75232 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 75232 | 70210 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 75232 | 59364 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 5340-00-679-3288
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225 TO 6, ALLOY 2024 FED SPEC SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT | ANODIZE |
| OVERALL HEIGHT | 0.1100 INCHES MINIMUM AND 0.1300 INCHES MAXIMUM |
| END DIAMETER | 0.6000 INCHES MINIMUM AND 0.6100 INCHES MAXIMUM |
| DISTANCE FROM END TO FIRST STEP | 0.0500 INCHES MINIMUM AND 0.0700 INCHES MAXIMUM |
| FIRST STEP DIAMETER | 0.7400 INCHES MINIMUM AND 0.7600 INCHES MAXIMUM |
| BORE DIAMETER | 0.1240 INCHES MINIMUM AND 0.1280 INCHES MAXIMUM |
| COUNTERBORE LENGTH | 0.0500 INCHES MINIMUM AND 0.0600 INCHES MAXIMUM |
| COUNTERBORE DIAMETER | 0.4400 INCHES MINIMUM AND 0.4600 INCHES MAXIMUM |
| DESIGN TYPE | SOLID |
| SPECIAL FEATURES | NOT CASEHARDENED |
| FSC APPLICATION DATA | FUEL PRESSURE REGULATORS,ENGINE,EXCEPT AIRCRAFT AND GUIDED MISSILE PRIME MOVING |