NSN 5340-00-624-4919 006244919
Product Details | HELICAL COMPRESSION SPRING SEAT
5340-00-624-4919 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.
Part Alternates: 006244919
Engines, Turbines, and Components | Gasoline Reciprocating Engines, Except Aircraft; and Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | 00-624-4919 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
Drawings & Photos | NSN 2805-00-624-4919
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Technical Data | NSN 5340-00-624-4919
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL HARDNESS RATING | NOT RATED |
| STYLE DESIGNATOR | N6 SEAT |
| OVERALL HEIGHT | 0.5150 INCHES MINIMUM AND 0.5400 INCHES MAXIMUM |
| END DIAMETER | 0.5630 INCHES NOMINAL |
| DISTANCE FROM END TO FIRST STEP | 0.4350 INCHES MINIMUM AND 0.4600 INCHES MAXIMUM |
| FIRST STEP DIAMETER | 1.2171 INCHES MINIMUM AND 1.2810 INCHES MAXIMUM |
| BORE DIAMETER | 0.4780 INCHES MINIMUM AND 0.4810 INCHES MAXIMUM |
| COUNTERBORE LENGTH | 0.1850 INCHES MINIMUM AND 0.1950 INCHES MAXIMUM |
| COUNTERBORE DIAMETER | 0.7500 INCHES NOMINAL |
| BORE TAPER IN DEG | 14.250 |
| DESIGN TYPE | SOLID |
| SPECIAL FEATURES | NOT CASEHARDENED;MATL-STEEL QQ-S-698 COMP FS0 |
| III FSC APPLICATION DATA | ENGINE,GASOLINE,NON-AIRCRAFT |
| MANUFACTURERS CODE | 24617 |
| DESIGN CONTROL REFERENCE | 837801 |
Restrictions/Controls & Freight Information | NSN 5340-00-624-4919
| Category | Code | Description |
|---|---|---|
| Hazardous Material Indicator Code | N | There is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials |
| Category | Code | Description |
|---|---|---|
| No Freight Information | ||