NSN 5307-01-521-1813

Part Details | SHOULDERED STUD

5307-01-521-1813 A headless fastener not exceeding 12 inches (304.8 mm) in length, threaded externally on both ends with threads of the same nominal diameter. All or part of the unthreaded section has a cross-sectional diameter greater than the nominal stud size plus 0.020 inches (0.508 mm). It may be thread relieved. See also STUD, LOCKED IN.

Alternate Parts: HL146638, HL146-6-3-8, 3M917338, 3M917-3-3-8, HL146638, HL146-6-3-8, HL146638, HL146-6-3-8, HL146638, HL146-6-3-8, 10116483, HL146638, HL146-6-3-8, HL146638, HL146-6-3-8, AICL146338, AIC-L-146-3-3-8, 5307-01-521-1813, 01-521-1813, 5307015211813, 015211813

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53JUN 14, 200401-521-181315946 ( STUD, SHOULDERED )
REFERENCE DRAWINGS & PICTURES

SHOULDERED

Cross Reference | NSN 5307-01-521-1813
Part Number Cage Code Manufacturer
HL146-6-3-892215ARCONIC GLOBAL FASTENERS & RINGS,INC.
3M917-3-3-876301BOEING COMPANY, THEDBA BOEING
HL146-6-3-873197HI-SHEAR CORPORATION
HL146-6-3-817446HUCK INTERNATIONAL, INC.DBA ARCONIC FASTENING SYSTEMS AND
HL146-6-3-8L4528LISI AEROSPACE CANADA CORPDIV HI SHEAR HOLDINGS INC
10116483A486GNIMIKKEISTOKESKUS NCB FINLAND
HL146-6-3-856878SPS TECHNOLOGIES, LLCDBA AEROSPACE DIVISION
HL146-6-3-806725SPS TECHNOLOGIES, LLCDBA AIR INDUSTRIES
AIC-L-146-3-3-806725SPS TECHNOLOGIES, LLCDBA AIR INDUSTRIES
Technical Data | NSN 5307-01-521-1813
Characteristic Specifications
MATERIAL TITANIUM ALLOY UNS R54520
MATERIAL DOCUMENT AND CLASSIFICATIONAAMS 4928$AAMS 4967 ALL MATERIAL RESPONSES
STYLE DESIGNATOR SHOULDERED
SHOULDER DIAMETER0.357 INCHES MINIMUM AND 0.377 INCHES MAXIMUM
SHOULDER LENGTH0.064 INCHES MINIMUM AND 0.074 INCHES MAXIMUM
NUT END SHANK LENGTH0.182 INCHES MINIMUM AND 0.192 INCHES MAXIMUM
STUD END SHANK LENGTH0.495 INCHES MINIMUM AND 0.505 INCHES MAXIMUM
STUD END SHANK DIAMETER0.188 INCHES MINIMUM AND 0.189 INCHES MAXIMUM
NUT END SHANK DIAMETER0.188 INCHES MINIMUM AND 0.189 INCHES MAXIMUM
OVERALL LENGTH1.391 INCHES MINIMUM AND 1.421 INCHES MAXIMUM
SPECIAL FEATURESLUBRICANT CETYL ALCOHOL
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONF-18 E/F AIRCRAFT
PART NAME ASSIGNED BY CONTROLLING AGENCYPIN-RIVET,THREADED-SHEAR,PROTRUDING HEAD,HEX POINT DRIVE,TITANIUM ALLOY