NSN 5340-01-125-0523

Part Details | HELICAL COMPRESSION SPRING SEAT

5340-01-125-0523 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: 1B481401, 1B48140-1, 10112446, 1B481401, 1B48140-1, 5340-01-125-0523, 01-125-0523, 5340011250523, 011250523

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53JAN 20, 198201-125-052324328 ( SEAT, HELICAL COMPRESSION SPRING )
REFERENCE DRAWINGS & PICTURES

SEAT

Cross Reference | NSN 5340-01-125-0523
Part Number Cage Code Manufacturer
1B48140-118355BOEING COMPANY, THEDBA BOEING
10112446A486GNIMIKKEISTOKESKUS NCB FINLAND
1B48140-181873WOODWARD HRT, INC.
Technical Data | NSN 5340-01-125-0523
Characteristic Specifications
MATERIAL STEEL COMP 304
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-S-763, CLASS 304, COND A FED SPEC SINGLE MATERIAL RESPONSE
SURFACE TREATMENT PASSIVATE
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONPS13001, MCDONNELL DOUGLAS CORP MFR REF SINGLE TREATMENT RESPONSE
STYLE DESIGNATOR SEAT
OVERALL HEIGHT0.5660 INCHES NOMINAL
END DIAMETER0.2170 INCHES MINIMUM AND 0.2220 INCHES MAXIMUM
DISTANCE FROM END TO FIRST STEP0.4400 INCHES NOMINAL
FIRST STEP DIAMETER0.6160 INCHES MINIMUM AND 0.6200 INCHES MAXIMUM
FIRST STEP LENGTH0.0360 INCHES MINIMUM AND 0.0380 INCHES MAXIMUM
SECOND END DIAMETER0.5450 INCHES MINIMUM AND 0.5490 INCHES MAXIMUM
BORE DIAMETER0.1920 INCHES MINIMUM AND 0.2020 INCHES MAXIMUM
CHAMFER ANGLE IN DEG45.0
DESIGN TYPE SOLID
SPECIAL FEATURESNOT CASEHARDENED
FSC APPLICATION DATACYLINDER ASSEMBLY,ACTUATING LINEAR,AIRCRAFT