Request a Quote for Boeing Company The Part Number ST9M580C1LW with the NSN 5340-01-105-6679

Part Number: ST9M580C1LW

Manufacturer: Boeing Company The

NSN: 5340-01-105-6679

NIIN: 011056679

Item Name : Bracket Angle

CAGE Code: 76301

FSC: 5340 Hardware Commercial

FSG: 53 Hardware and Abrasives

Country : USA

NCB Code : 01

Maintenance Parts Pro is pleased to offer procurement options for Boeing Company The part number ST9M580C1LW, a Bracket Angle product we carry that is listed with the NSN 5340-01-105-6679 for seamless identification. As this item is available for purchase today, be sure to fill out and submit the Request for Quote (RFQ) form on this page if you are interested in obtaining pricing information. All that we ask is that you share details like your budget, desired quantity, and expected fulfillment speed so that we can respond with the most fitting solutions for your comparisons.

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Alongside streamlined quotation processes, we aim to support our customers by providing as much relevant listing information and data with product offerings as possible. For example, part number ST9M580C1LW specifically traces back to Boeing Company The through CAGE Code 76301, as well as belongs to the FSC [FSC] as per its NSN of 5340-01-105-6679. Referencing such details, you can locate and procure exact specifications with ease. With our various practices in mind, do not hesitate to request a quote on part number ST9M580C1LW using our provided form.

NSN Information for Part Number ST9M580C1LW with NSN 5340-01-105-6679, 5340011056679

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
5340-01-105-6679 Item PartTypeName: BRACKET,ANGLE	5340	011056679	0	P
	CIIC	HCC	ESD	PMIC	Criticality	ENAC
	U			A	0
Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
ST9M580C1R	5	9	5

Characteristics Data of NSN 5340-01-105-6679, 5340011056679

MRC	Criteria	Characteristic
ADLK	FIRST LEG LENGTH	0.750 INCHES NOMINAL
ADLL	SECOND LEG LENGTH	0.750 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	W/S: AIRCRAFT,HARRIER AV-8B; AIRCRAFT,EAGLE F-15; AIRCRAFT,HORNET F/A-18; F/A-18E/F HORNET AIRCRAFT; AVIATION ORDANCE; GUN SYSTEM,25MM
AHLF	SECOND LEG WIDTH	0.980 INCHES MINIMUM AND 1.020 INCHES MAXIMUM
AHLG	SECOND LEG CORNER RADIUS	0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM
AHLK	FIRST LEG HOLE DIAMETER	0.129 INCHES MINIMUM AND 0.134 INCHES MAXIMUM
AHLN	SECOND LEG HOLE DIAMETER	0.220 INCHES MINIMUM AND 0.230 INCHES MAXIMUM
AHLV	SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH	0.230 INCHES MINIMUM AND 0.250 INCHES MAXIMUM
AHLW	SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH	0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM
AHPW	FIRST LEG THICKNESS	0.050 INCHES NOMINAL
AHPX	SECOND LEG THICKNESS	0.050 INCHES NOMINAL
AHQN	FIRST LEG WIDTH	0.980 INCHES MINIMUM AND 1.020 INCHES MAXIMUM
AHQP	FIRST LEG CORNER RADIUS	0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM
AHQU	FIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH	0.490 INCHES MINIMUM AND 0.510 INCHES MAXIMUM
AHRA	FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH	0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM
AHRB	FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH	0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM
AJZU	FIRST LEG STYLE	CORNER RADIUS
AKAU	FIRST LEG HOLE ARRANGEMENT STYLE	TWO HOLES
AKBU	SECOND LEG STYLE	CORNER RADIUS
AKCU	SECOND LEG HOLE ARRANGEMENT STYLE	TWO HOLES
CSSP	SECOND LEG RELATIONSHIP TO FIRST LEG	NOT IDENTICAL
CSSQ	FIRST LEG ANGLE	90.0 DEGREES NOMINAL
MATT	MATERIAL	ALUMINUM ALLOY 2024
MDCL	MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5,T81 FED SPEC SINGLE MATERIAL RESPONSE
SFTT	SURFACE TREATMENT	PAINT
STDC	SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	MIL-P-23377 MIL SPEC SINGLE TREATMENT RESPONSE
STYL	STYLE DESIGNATOR	ANGLE