NSN 5340-00-942-2509

Part Details | HELICAL COMPRESSION SPRING SEAT

5340-00-942-2509 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: 731313, 5340-00-942-2509, 00-942-2509, 5340009422509, 009422509

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53DEC 11, 196500-942-250924328 ( SEAT, HELICAL COMPRESSION SPRING )
REFERENCE DRAWINGS & PICTURES

SEAT

Cross Reference | NSN 5340-00-942-2509
Part Number Cage Code Manufacturer
73131396124TRANSDIGM, INC.DBA AERO FLUID PRODUCTS
Technical Data | NSN 5340-00-942-2509
Characteristic Specifications
MATERIAL ALUMINUM ALLOY
SURFACE TREATMENT ANODIZE
STYLE DESIGNATOR SEAT
OVERALL HEIGHT0.3650 INCHES NOMINAL
END DIAMETER0.3650 INCHES NOMINAL
DISTANCE FROM END TO FIRST STEP0.1300 INCHES NOMINAL
FIRST STEP DIAMETER0.4294 INCHES MINIMUM AND 0.4375 INCHES MAXIMUM
BORE DIAMETER0.2800 INCHES NOMINAL
COUNTERSINK DIAMETER0.1870 INCHES NOMINAL
COUNTERBORE LENGTH0.5000 INCHES NOMINAL
COUNTERBORE DIAMETER0.4174 INCHES MINIMUM AND 0.4255 INCHES MAXIMUM
COUNTERSINK ANGLE IN DEG90.0
CHAMFER ANGLE IN DEG45.0
DESIGN TYPE SOLID
FSC APPLICATION DATAAIRCRAFT ENGINE FUEL CONTROL SYSTEM