NSN 5305-00-216-8523

Part Details | SOCKET HEAD CAP SCREW

5305-00-216-8523 An externally threaded fastener whose threaded portion is of one nominal diameter. The head has an internal socket or multiple spline for use with an inserted driver. A locking feature may be incorporated in the design of the head or threads. Excludes items with bevel (conical) heads. See BOLT, INTERNAL WRENCHING. Excludes SCREW, SHOULDER; and SCREW, MACHINE.

Alternate Parts: 32457858, 324578-58, NAS1352C022, NAS1352C02-2, 5305-00-216-8523, 00-216-8523, 5305002168523, 002168523

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53MAY 02, 197300-216-852316282 ( SCREW, CAP, SOCKET HEAD )
REFERENCE DRAWINGS & PICTURES

CROWNED HEXAGON

HEXAGON

Cross Reference | NSN 5305-00-216-8523
Part Number Cage Code Manufacturer
324578-5807187HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
NAS1352C02-280205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
Technical Data | NSN 5305-00-216-8523
Characteristic Specifications
THREAD SERIES DESIGNATOR UNJC
NOMINAL THREAD DIAMETER0.086 INCHES
THREAD QUANTITY PER INCH56
THREAD CLASS3A
THREAD DIRECTION RIGHT-HAND
THREAD LENGTH0.073 INCHES MINIMUM AND 0.141 INCHES MAXIMUM
FASTENER LENGTH0.109 INCHES MINIMUM AND 0.141 INCHES MAXIMUM
MINIMUM TENSILE STRENGTH80000 POUNDS PER SQUARE INCH
MINIMUM YIELD STRENGTH30000 POUNDS PER SQUARE INCH
HEAD STYLE9 CROWNED HEXAGON
HEAD DIAMETER0.134 INCHES MINIMUM AND 0.140 INCHES MAXIMUM
HEAD HEIGHT0.083 INCHES MINIMUM AND 0.086 INCHES MAXIMUM
INTERNAL DRIVE STYLE HEXAGON
WIDTH ACROSS FLATS0.078 INCHES MINIMUM AND 0.079 INCHES MAXIMUM
SPECIFICATION/STANDARD DATA80205-NAS1352 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD
END ITEM IDENTIFICATIONW/S: AIRCRAFT, TOMCAT F-14; AIRCRAFT, STRATOFORTRESS B-52; HELICOPTER, CH-53A/D/E; AIRCRAFT, HAWKEYE E-2C; HELICOPTER, RH-53; HELICOPTER, MH-53E; HELICOPTER OBSERVATION (AHIP), OH-58D; AIRCRAFT, C-2A (REPROCURED); MISSILE, ADVANCED MEDIUM RANGE AIR-TO-AIR (AMRAAM)/AIM120A