Request a Quote on Boeing Company The Part L3223760-059 with the NSN 1560-01-592-9806

Part Number: L3223760-059

Alternate P/N: L3223760059

Manufacturer: Boeing Company The

NSN: 1560-01-592-9806

NIIN: 015929806

Item Name : Web Structural Component Aircraf

CAGE Code: 43999

FSC: 1560 Airframe Structural Components

FSG: 15 Aircraft and Airframe Structural Components

Country : USA

NCB Code : 01

Thank you for taking interest in Boeing Company The part number L3223760-059, which is listed with the NSN 1560-01-592-9806 and a product description of “Web Structural Component Aircraf.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.

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NSN Information for Part Number L3223760-059 with NSN 1560-01-592-9806, 1560015929806

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
1560-01-592-9806 Item PartTypeName: WEB,STRUCTURAL COMPONENT,AIRCRAF	1560	015929806	0	P	A
	CIIC	HCC	ESD	PMIC	Criticality	ENAC
	7		A	A	0
Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
L3223760-059	5	2	3

Characteristics Data of NSN 1560-01-592-9806, 1560015929806

MRC	Criteria	Characteristic
ABHP	OVERALL LENGTH	10.100 INCHES NOMINAL
ABMK	OVERALL WIDTH	3.000 INCHES NOMINAL
ABPX	MATERIAL THICKNESS	0.050 INCHES NOMINAL
CRTL	CRITICALITY CODE JUSTIFICATION	FEAT
CXCY	PART NAME ASSIGNED BY CONTROLLING AGENCY	WEB, PIVOTING WEDGE
CZDJ	AIRCRAFT LOCATION	UNDERWING FAIRING
CZEK	AIRCRAFT MISSION DESIGN SERIES	B-1B
FEAT	SPECIAL FEATURES	HARDNESS CRITICAL ITEM;OPPOSITE -060
MATT	III MATERIAL	ALUMINUM ALLOY 2024
MDCL	MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5 FED STD SINGLE MATERIAL RESPONSE