NSN 5340-00-775-1855
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-00-775-1855 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: 114C12463, 114C1246-3, 114C12463, 114C1246-3, 5340-00-775-1855, 00-775-1855, 5340007751855, 007751855
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1960 | 00-775-1855 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
SEAT
Cross Reference | NSN 5340-00-775-1855
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 114C1246-3 | 81205 | THE BOEING COMPANYDBA BOEING |
| 114C1246-3 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 5340-00-775-1855
| Characteristic | Specifications |
|---|---|
| MATERIAL | 1$1$EALUMINUM ALLOY,QQ-A-200 TO 8,6061,T6510 OR T6511 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 8, 6061, T651 FED SPEC 1ST MATERIAL RESPONSE AND MIL-A-22771, 6061, T652 MIL SPEC 2ND MATERIAL RESPONSE |
| STYLE DESIGNATOR | SEAT |
| OVERALL HEIGHT | 0.7500 INCHES NOMINAL |
| END DIAMETER | 0.7800 INCHES NOMINAL |
| DISTANCE FROM END TO FIRST STEP | 0.2500 INCHES NOMINAL |
| FIRST STEP DIAMETER | 1.3750 INCHES MINIMUM AND 1.3850 INCHES MAXIMUM |
| BORE DIAMETER | 0.4520 INCHES MINIMUM AND 0.4600 INCHES MAXIMUM |
| DESIGN TYPE | SOLID |
| FSC APPLICATION DATA | SPRING ASSEMBLY PITCH |