Recently Updated NSN 9535-01-532-0309 Or (9535015320309) Part List

Item Name	Sheet Metal
Federal Supply Group (FSG)	Metal Bars Sheets and Shapes
Federal Supply Class (FSC)	9535 Plate Sheet Strip and Foil Nonferrous Base Metal
National Item Identification Number (NIIN)	01-532-0309 (015320309)
NCB Code	USA (01)
Manufacturer	Society Of Automotive Engineers Inc, Sae International

Part Number	Manufacturer	Item Name	RFQ
AMS-QQ-A-250 5-O-0.100X12X48	society of automotive engineers inc	sheet metal	RFQ
AMS-QQ-A-250 5	sae international	sheet metal	RFQ
AMS-QQ-A-250 5-CD0-0 1X12X48	society of automotive engineers inc	sheet metal	RFQ
AMS-QQ-A-250 5-O-0.100X12X48	sae international	sheet metal	RFQ
AMS-QQ-A-250 5	society of automotive engineers inc	sheet metal	RFQ

MRC	Criteria	Characteristic
AARN	FABRICATION METHOD	ROLLED
ABGL	WIDTH	12.000 INCHES NOMINAL
ABRY	LENGTH	48.000 INCHES NOMINAL
ADVM	CROSS-SECTIONAL THICKNESS	0.1000 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
AGTA	BASIC SHAPE STYLE	SOLID
ALBY	USAGE DESIGN	AIRCRAFT
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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS;
HEAT	HEAT TREATMENT	O-ANNEALED
MATL	MATERIAL	ALUMINUM ALLOY, QQ-A-250/5
AARN	FABRICATION METHOD	ROLLED
ABGL	WIDTH	12.000 INCHES NOMINAL
ABRY	LENGTH	48.000 INCHES NOMINAL
ADVM	CROSS-SECTIONAL THICKNESS	0.1000 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
AGTA	BASIC SHAPE STYLE	SOLID
ALBY	USAGE DESIGN	AIRCRAFT
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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS;
HEAT	HEAT TREATMENT	O-ANNEALED
MATL	MATERIAL	ALUMINUM ALLOY, QQ-A-250/5