NSN 5340-00-488-6875
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-00-488-6875 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: 2004T97P01, 5340-00-488-6875, 00-488-6875, 5340004886875, 004886875
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | MAR 11, 1972 | 00-488-6875 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5340-00-488-6875
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2004T97P01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 5340-00-488-6875
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| OVERALL HEIGHT | 0.1900 INCHES MINIMUM AND 0.2100 INCHES MAXIMUM |
| END DIAMETER | 0.2900 INCHES MINIMUM AND 0.3000 INCHES MAXIMUM |
| DISTANCE FROM END TO FIRST STEP | 0.1600 INCHES MINIMUM AND 0.1700 INCHES MAXIMUM |
| FIRST STEP DIAMETER | 0.3900 INCHES MINIMUM AND 0.4100 INCHES MAXIMUM |
| DESIGN TYPE | SOLID |
| FSC APPLICATION DATA | FUEL CONTROL,ENGINE,AIRCRAFT |