Quote on AMS-T-9046-COMPCP-1-0.032X36X96 of Society Of Automotive Engineers Inc with NSN 9535015323832

Part Number: AMS-T-9046-COMPCP-1-0.032X36X96

Alternate P/N: AMST9046COMPCP10032X36X96

Manufacturer: Society Of Automotive Engineers Inc

NSN: 9535-01-532-3832

NIIN: 015323832

Item Name : Sheet Metal

CAGE Code: 81343

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 Vital Purchasing, we prioritize providing our customers with only the highest quality NSN parts and services. As such, we proudly source all of our components such as part number AMS-T-9046-COMPCP-1-0.032X36X96 from leading manufacturers like Society Of Automotive Engineers Inc, an entity that operates with CAGE Code 81343. More than that, we subject countless items to thorough quality assurance measures to guarantee their caliber prior to purchase, and we boast a global supply-chain network that allows us to expedite shipping times for both domestic and international orders to accommodate those with rigid time constraints. Begin the procurement process for all the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal related parts you require today to see how we can simplify part sourcing for you.

NSN Information for Part Number AMS-T-9046-COMPCP-1-0.032X36X96 with NSN 9535-01-532-3832, 9535015323832

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
9535-01-532-3832 Item PartTypeName: SHEET,METAL	9535	015323832		N	A
	CIIC	HCC	ESD	PMIC	Criticality	ENAC
			A	A	0
Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
AMS-T-9046	5	1	3

Characteristics Data of NSN 9535-01-532-3832, 9535015323832

MRC	Criteria	Characteristic
AARN	FABRICATION METHOD	ANY ACCEPTABLE
ABGL	WIDTH	36.000 INCHES NOMINAL
ABRY	LENGTH	96.000 INCHES NOMINAL
ADVM	CROSS-SECTIONAL THICKNESS	0.0320 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
AGTA	BASIC SHAPE STYLE	SOLID
CQBC	MINIMUM TENSILE STRENGTH	80000 POUNDS PER SQUARE INCH
CQHQ	MINIMUM YIELD STRENGTH	70000 POUNDS PER SQUARE INCH
FEAT	SPECIAL FEATURES	MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT
HEAT	HEAT TREATMENT	ANNEALED
MATL	MATERIAL	TITANIUM
AARN	FABRICATION METHOD	ANY ACCEPTABLE
ABGL	WIDTH	36.000 INCHES NOMINAL
ABRY	LENGTH	96.000 INCHES NOMINAL
ADVM	CROSS-SECTIONAL THICKNESS	0.0320 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
AGTA	BASIC SHAPE STYLE	SOLID
CQBC	MINIMUM TENSILE STRENGTH	80000 POUNDS PER SQUARE INCH
CQHQ	MINIMUM YIELD STRENGTH	70000 POUNDS PER SQUARE INCH
FEAT	SPECIAL FEATURES	MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT
HEAT	HEAT TREATMENT	ANNEALED
MATL	MATERIAL	TITANIUM