NSN 9535-01-531-7795 (9535015317795) Listing

Alternative NSN: 9535-01-531-7795

Item Name: Sheet Metal

FSG: 95 Metal Bars Sheets and Shapes

Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal

NCB Code: USA (01)

Manufacturers: Sae International, Society Of Automotive Engineers Inc

Browse NSN parts of NSN 9535-01-531-7795 and get lowest price for your requested parts in 15 minutes. Just ordered part of NSN 9535-01-531-7795 like AMS-QQ-A-250 5, AMS-QQ-A-250 5, AMS-QQ-A-250 5-CDT81-0 04X12X36, AMS-QQ-A-250 5-T81-0.040X12X36, AMS-QQ-A-250 5-T81-0.040X12X36 described as Sheet Metal from industry leading manufactures such as Society Of Automotive Engineers Inc, Sae International. We are proud to offer an inventory of over 2 billion ready-to-ship parts, 24/7 availability, and key locations in the U.S./abroad. These attributes allow us to meet all aircraft on ground (AOG) requirements with ease.

Part Number's List for NSN 9535-01-531-7795, 9535015317795

Part No	Manufacturer	Item Name	QTY	RFQ
AMS-QQ-A-250 5	Society Of Automotive Engineers Inc	sheet metal	Avl	RFQ
AMS-QQ-A-250 5	Sae International	sheet metal	Avl	RFQ
AMS-QQ-A-250 5-CDT81-0 04X12X36	Society Of Automotive Engineers Inc	sheet metal	Avl	RFQ
AMS-QQ-A-250 5-T81-0.040X12X36	Society Of Automotive Engineers Inc	sheet metal	Avl	RFQ
AMS-QQ-A-250 5-T81-0.040X12X36	Sae International	sheet metal	Avl	RFQ

Product Specification of NSN 9535015317795

MRC	Criteria	Characteristic
AARN	FABRICATION METHOD	ROLLED
ABGL	WIDTH	12.000 INCHES NOMINAL
ABRY	LENGTH	36.000 INCHES NOMINAL
ADVM	CROSS-SECTIONAL THICKNESS	0.0400 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
AGTA	BASIC SHAPE STYLE	SOLID
ALBY	USAGE DESIGN	AIRCRAFT
CQBC	MINIMUM TENSILE STRENGTH	62000 POUNDS PER SQUARE INCH
CQHQ	MINIMUM YIELD STRENGTH	54000 POUNDS PER SQUARE INCH
FEAT	SPECIAL FEATURES	THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS
HEAT	HEAT TREATMENT	T-81 SOLUTION HEAT TREATED
MATL	MATERIAL	ALUMINUM ALLOY, QQ-A-250/5
AARN	FABRICATION METHOD	ROLLED
ABGL	WIDTH	12.000 INCHES NOMINAL
ABRY	LENGTH	36.000 INCHES NOMINAL
ADVM	CROSS-SECTIONAL THICKNESS	0.0400 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
AGTA	BASIC SHAPE STYLE	SOLID
ALBY	USAGE DESIGN	AIRCRAFT
CQBC	MINIMUM TENSILE STRENGTH	62000 POUNDS PER SQUARE INCH
CQHQ	MINIMUM YIELD STRENGTH	54000 POUNDS PER SQUARE INCH
FEAT	SPECIAL FEATURES	THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS
HEAT	HEAT TREATMENT	T-81 SOLUTION HEAT TREATED
MATL	MATERIAL	ALUMINUM ALLOY, QQ-A-250/5

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