Find Part Number AMS-T-9046-COMPCP-1-0.020X36X96 With NSN 9535-01-532-3824 by Sae International!

Part Number: AMS-T-9046-COMPCP-1-0.020X36X96

Alternate P/N: AMST9046COMPCP10020X36X96

Manufacturer: Sae International

NSN: 9535-01-532-3824

NIIN: 015323824

Item Name : Sheet Metal

CAGE Code: 0U583

FSC: 9535 Plate Sheet Strip and Foil Nonferrous Base Metal

FSG: 95 Metal Bars Sheets and Shapes

Country: USA

NCB Code: 01

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At National Stock Numbers Quotes, we make it a priority to meet our customers’ operational requirements, so we keep catalogs fully stocked with in-demand NSN parts like those with the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal by Sae International. For additional specification regarding your part needs, you can also find a wide range of items by their respective CAGE Code, such as 0U583, and many other designations for your ease-of-search. Kick off the procurement process with a competitive quote for NSN 9535-01-532-3824 today and see why customers continuously rely on National Stock Numbers Quotes time and time again. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock!

NSN Information for Part Number AMS-T-9046-COMPCP-1-0.020X36X96 with NSN 9535-01-532-3824, 9535015323824

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
9535-01-532-3824 Item PartTypeName: SHEET,METAL	9535	015323824		N	A
	CIIC	HCC	ESD	PMIC	Criticality	ENAC
			A	A	0
Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
AMS-T-9046-COMPCP-1-0.020X36X96	5	9	5

Characteristics Data of NSN 9535-01-532-3824, 9535015323824

MRC	Criteria	Characteristic
ADVM	Cross-Sectional Thickness	0.0200 INCHES NOMINAL
MATT	Material	TITANIUM
HEAT	Heat Treatment	ANNEALED
CQHQ	Minimum Yield Strength	70000 POUNDS PER SQUARE INCH
AGTA	Basic Shape Style	SOLID
ABRY	Length	96.000 INCHES NOMINAL
ABGL	Width	36.000 INCHES NOMINAL
AGAV	End Item Identification	FUSELAGE F4F JET AIRCRAFT
MRC	Decoded Requirement	Clear Text Reply
CQBC	Minimum Tensile Strength	80000 POUNDS PER SQUARE INCH
FEAT	Special Features	MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT
AARN	Fabrication Method	ANY ACCEPTABLE