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NSN 5306-01-303-0912  ·  NIIN 013030912  ·  FSC 5306
NO DASHES 5306013030912
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BOLT,SHOULDER

Bolts

Application: F-16 AIRCRAFT

Technical characteristics

26 rows

Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.

Technical characteristics from the federal item record
MRCRequirementValue
AAJDTHREAD CLASS3A
AAJFTHREAD DIRECTIONRIGHT-HAND
AASATHREAD LENGTHINCHES NOMINAL 0.375
AASBFASTENER LENGTHINCHES NOMINAL 1.842
AASKHEAD STYLE
AASUHEAD HEIGHTINCHES MINIMUM 0.172 AND INCHES MAXIMUM 0.204
AATBWIDTH BETWEEN FLATSINCHES MINIMUM 0.492 AND INCHES MAXIMUM 0.502
AATNSHOULDER DIAMETERFIRST SHOULDER INCHES MINIMUM 0.3735 AND INCHES MAXIMUM 0.3745
AATXSHOULDER LENGTHFIRST SHOULDER INCHES NOMINAL 1.467
AAWBSHANK UNTHREADED HOLE DIAMETERFIRST HOLE INCHES MINIMUM 0.076 AND INCHES MAXIMUM 0.086
AGAVEND ITEM IDENTIFICATIONF-16 AIRCRAFT
AHYMNOMINAL THREAD DIAMETERINCHES 0.312
CMLPTHREAD QUANTITY PER INCH24
CQBCMINIMUM TENSILE STRENGTHPOUNDS PER SQUARE INCH 220000
CQFMHARDNESS RATINGOVERALL ROCKWELL C MINIMUM 46.0 AND ROCKWELL C MAXIMUM 50.0
CRZSDISTANCE FROM HEAD LARGEST BEARING SURFACE TO SHANK HOLE CENTERFIRST HOLE INCHES NOMINAL 1.682
CWYBSHOULDER SHAPEFIRST SHOULDER ROUND
MATTMATERIALOVERALL STEEL COMP H11
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONOVERALL ASSN STD SINGLE MATERIAL RESPONSE A-S 6485 OR ASSN STD SINGLE MATERIAL RESPONSE A-S 6487
SFTTSURFACE TREATMENTTHREADS CADMIUM AND CHROMATE
SFTTSURFACE TREATMENTGRIP CHROMIUM
SFTTSURFACE TREATMENTHEAD CADMIUM AND CHROMATE
STDCSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONHEAD FED SPEC SINGLE TREATMENT RESPONSE QQ--416 TY 2
STDCSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONGRIP FED SPEC SINGLE TREATMENT RESPONSE QQ-C-320 TY 2
STDCSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONTHREADS FED SPEC SINGLE TREATMENT RESPONSE QQ--416 TY 2
THSDTHREAD SERIES DESIGNATORUNIFIED NATIONAL JOINT FINE (UNJF)