National Stock Number (NSN) 9535-01-532-0298 (9535015320298) Parts 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)	01-532-0298 (015320298)
NCB Code	USA (01)
Manufacturer	Sae International, Society Of Automotive Engineers Inc

Part Number	Manufacturer	Item Name	Cage Code	RFQ
AMS-QQ-A-250 5-O-0.040X12X36	sae international	sheet metal	0u583	RFQ
AMS QQ A 250 5	society of automotive engineers inc	sheet metal	81343	RFQ
AMS-QQ-A-250 5-CD0-0 04X12X36	society of automotive engineers inc	sheet metal	81343	RFQ
AMS-QQ-A-250 5	sae international	sheet metal	0u583	RFQ
AMS-QQ-A-250 5-O-0.040X12X36	society of automotive engineers inc	sheet metal	81343	RFQ

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
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	O-ANNEALED
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
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	O-ANNEALED
MATL	MATERIAL	ALUMINUM ALLOY, QQ-A-250/5