NSN 5340-01-355-0272
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-01-355-0272 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: 55982721, 5598272-1, 55982721, 5598272-1, 5340-01-355-0272, 01-355-0272, 5340013550272, 013550272
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | MAR 10, 1992 | 01-355-0272 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
SEAT
Cross Reference | NSN 5340-01-355-0272
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5598272-1 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 5598272-1 | 53711 | NAVAL SEA SYSTEMS COMMAND |
Technical Data | NSN 5340-01-355-0272
| Characteristic | Specifications |
|---|---|
| SURFACE TREATMENT | ANODIZE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 TY 3 CL 1 MIL SPEC SINGLE TREATMENT RESPONSE |
| STYLE DESIGNATOR | 7 SEAT |
| OVERALL HEIGHT | 0.7300 INCHES NOMINAL |
| END DIAMETER | 1.1500 INCHES NOMINAL |
| DISTANCE FROM END TO FIRST STEP | 0.3900 INCHES NOMINAL |
| BORE DIAMETER | 0.9400 INCHES NOMINAL |
| DESIGN TYPE | SOLID |