NSN 5340-00-354-7954
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-00-354-7954 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: 4021692, 4021692, 5340-00-354-7954, 00-354-7954, 5340003547954, 003547954
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | FEB 06, 1974 | 00-354-7954 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5340-00-354-7954
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4021692 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4021692 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-354-7954
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL COMP 410 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5613 ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL HARDNESS RATING | RCB25.0 ROCKWELL C MAXIMUM AND 233.0 ROCKWELL C MAXIMUM |
| DESIGN TYPE | SOLID |
| FSC APPLICATION DATA | ENGINE,AIRCRAFT,TURBOFAN |