Quote for BACB30NF8D5 With NSN 5306-01-204-6843 of Boeing Company (CAGE Code 81205)

Mfg Part Number: BACB30NF8D5	NSN : 5306-01-204-6843
NIIN : 012046843	CAGE Code : 81205
Manufacturer: Boeing Company	Item Name : Bolt Close Tolerance
FSC : 5306 Bolts

Thank you for your interest in BACB30NF8D5 part of with NSN 5306-01-204-6843 having CAGE Code 81205 under FSC 5306 Bolts manufactured by Boeing Company. You have reached our RFQ page for BACB30NF8D5 part, and completing the form below will allow you to request a quote on this Boeing Company product for your comparisons. As you complete our offered form, we ask that you provide us with as much information regarding your needs as you can for the NSN part BACB30NF8D5, so that we may best personalize a solution that is fit for you. 012046843 81205 5306 Bolts Bolt Close Tolerance

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NSN Information for Part Number BACB30NF8D5 with NSN 5306-01-204-6843, 5306012046843

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
5306-01-204-6843 Item Description: BOLT,CLOSE TOLERANCE	5306	012046843		N
	CIIC	HCC	ESD	PMIC	Criticality	ENAC

Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
BACB30NF8D5	5	2	3

Characteristics Data of NSN 5306-01-204-6843, 5306012046843

MRC	Criteria	Characteristic
AAJF	THREAD DIRECTION	RIGHT-HAND
AASB	FASTENER LENGTH	0.888 INCHES MINIMUM AND 0.938 INCHES MAXIMUM
AASU	HEAD HEIGHT	0.250 INCHES MINIMUM AND 0.265 INCHES MAXIMUM
AAUR	GRIP DIAMETER	0.4985 INCHES MINIMUM AND 0.4995 INCHES MAXIMUM
AHYM	NOMINAL THREAD DIAMETER	0.500 INCHES
CMLP	THREAD QUANTITY PER INCH	20
CXCY	PART NAME ASSIGNED BY CONTROLLING AGENCY	BOLT HX HD
MDCL	MATERIAL DOCUMENT AND CLASSIFICATION	MIL-S-5000 MIL SPEC 1ST MATERIAL RESPONSE OVERALL OR AMS 6322 ASSN STD 2ND MATERIAL RESPONSE OVERALL
STDC	SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	QQ-P-416, TY 2, CL 2 FED SPEC ALL TREATMENT RESPONSES OVERALL
AAJD	THREAD CLASS	3A
AASA	THREAD LENGTH	0.526 INCHES MINIMUM AND 0.556 INCHES MAXIMUM
AASK	HEAD STYLE	UNDERCUT HEXAGON
AATB	WIDTH BETWEEN FLATS	0.741 INCHES MINIMUM AND 0.752 INCHES MAXIMUM
AGAV	END ITEM IDENTIFICATION	USED ON SENTRY F22 AIRCRAFT
ANEE	GRIP LENGTH	0.362 INCHES MINIMUM AND 0.382 INCHES MAXIMUM
CQBC	MINIMUM TENSILE STRENGTH	140000 POUNDS PER SQUARE INCH
MATT	MATERIAL	STEEL COMP 4340 OVERALL OR STEEL COMP 8740 OVERALL
SFTT	SURFACE TREATMENT	CADMIUM OVERALL
THSD	THREAD SERIES DESIGNATOR	UNJF