NSN 5340-01-187-8416
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-01-187-8416 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: L5877112003, L5877112-003, 5340-01-187-8416, 01-187-8416, 5340011878416, 011878416
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | AUG 26, 1984 | 01-187-8416 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5340-01-187-8416
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| L5877112-003 | 43999 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 5340-01-187-8416
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| DESIGN TYPE | SOLID |
| SPECIAL FEATURES | DIMENSIONS IN INCHES;0.6900 LONG,0.3580 DIAMETER 0.4400 LONG,GROOVED 0.1430 FROM FIRST END,0.2070 WIDE,0.2480 DIAMETER DEEP,FIRST END DRILLED 0.0890 SPHERICAL BOTTOM HOLE DEPTH 90 DEGREE COUNTER-SUNK 0.1120-40UNJC-3B DIAMETER THREADS;SECOND END 0.0780 DIAMETER;0.2500 LONG |
| FSC APPLICATION DATA | AIRCRAFT HYDRAULIC SYSTEMS |