NSN 5340-01-347-8677
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-01-347-8677 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: 184244001, 184244-001, 184244001, 184244-001, 184244001, 184244-001, 5340-01-347-8677, 01-347-8677, 5340013478677, 013478677
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | OCT 30, 1991 | 01-347-8677 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
SEAT
Cross Reference | NSN 5340-01-347-8677
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 184244-001 | 0UES3 | MOOG INC. |
| 184244-001 | 94697 | MOOG INC.DBA MOOG |
| 184244-001 | 19156 | MOOG INC.DIV MOOG AIRCRAFT, SALT LAKE |
Technical Data | NSN 5340-01-347-8677
| Characteristic | Specifications |
|---|---|
| MATERIAL | 5$EALUMINUM,QQ-A-200 TO 11,ALLOY 7075-T73 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225 TO 9, ALLOY 7075, T73 FED SPEC 1ST MATERIAL RESPONSE |
| SURFACE TREATMENT | ANODIZE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625, TYPE 2 MIL SPEC SINGLE TREATMENT RESPONSE |
| STYLE DESIGNATOR | 7 SEAT |
| OVERALL HEIGHT | 0.1550 INCHES NOMINAL |
| END DIAMETER | 0.6000 INCHES NOMINAL |
| DISTANCE FROM END TO FIRST STEP | 0.0900 INCHES NOMINAL |
| FIRST STEP DIAMETER | 1.2920 INCHES NOMINAL |
| BORE DIAMETER | 0.4000 INCHES NOMINAL |
| DESIGN TYPE | SOLID |