NSN 5306-01-501-2132

Part Details | SHOULDER BOLT

5306-01-501-2132 An externally threaded fastener whose threaded portion is of one nominal diameter, No. 10 (0.190 IN.) (5 mm) or larger. It has a round unthreaded neck or shank all or part of which is of greater diameter than the threaded portion. The head is not designed to be held or driven with an inserted drivers. A locking feature may be incorporated in the design of the head or threads. For items with a thread diameter smaller than No. 10 (0.190 IN.) (5 mm) and those items with an inserted drive head, use SCREW, SHOULDER. For items which are No. 10 (0.190 IN.) (5 mm) or larger in size and are both shouldered and have an externally relieved body, use BOLT, EXTERNALLY RELIEVED BODY. Excludes THUMBSCREW.

Alternate Parts: BACB30PW358, BACB30PW3-58, 5306-01-501-2132, 01-501-2132, 5306015012132, 015012132

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53SEP 26, 200201-501-213204905 ( BOLT, SHOULDER )
REFERENCE DRAWINGS & PICTURES

HEXAGON

Cross Reference | NSN 5306-01-501-2132
Part Number Cage Code Manufacturer
BACB30PW3-5881205THE BOEING COMPANYDBA BOEING
Technical Data | NSN 5306-01-501-2132
Characteristic Specifications
THREAD SERIES DESIGNATOR UNJC
NOMINAL THREAD DIAMETER0.138 INCHES
THREAD QUANTITY PER INCH32
THREAD CLASS3A
THREAD DIRECTION RIGHT-HAND
THREAD LENGTH0.258 INCHES NOMINAL
FASTENER LENGTH4.058 INCHES NOMINAL
HEAD STYLE HEXAGON
HEAD HEIGHT0.125 INCHES NOMINAL
WIDTH BETWEEN FLATS0.371 INCHES NOMINAL
SPECIAL FEATURESCADMIUM PLATED BOLTS INTENDED FOR USE IN CONTACT WITH ALUMINUM ALLOY PARTS OR STRUCTURE
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONMV-22 AIRCRAFT (V-22 LRIP 1 E-NSN ISIL)
PART NAME ASSIGNED BY CONTROLLING AGENCYBOLT, HEX HEAD, SHOULDER, A286 CRES, LONG THREAD, SELF-LOCKING AND NONLOCKING; INAVY: BOLT, SHOULDER, AIRCRAFT