Browse NSN 9535-01-531-7783 Listing of Sheet Metal

It is our pleasure to inform you that part number AMS-QQ-A-250 5, AMS-QQ-A-250 5, AMS-QQ-A-250 5-CDT3-0 016X12X36, AMS QQ A 250 5 T3 0 016X12X36, AMS QQ A 250 5 T3 0 016X12X36 listed under NSN 9535-01-531-7783 is now available and ready to ship from Fulfillment By ASAP. This part described as a Sheet Metal manufactured by Sae Inc, Society Of Automotive Engineers Inc. If you’d like a quick quote for NSN 9535-01-531-7783, please fill out the form from below. Are you looking to have it delivered today or tomorrow? We can help! Simply complete the Request For Quote (RFQ) form given below to get started, and we will get back to you within 15 minutes!

Alternative NSN: 9535-01-531-7783

Item Name: Sheet Metal

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

NIIN: 015317783

NCB Code: USA (01)

Manufacturers: Sae Inc , Society Of Automotive Engineers Inc

Part No	Manufacturer	Item Name	QTY	RFQ
AMS-QQ-A-250 5	sae inc	sheet metal	Avl	RFQ
AMS-QQ-A-250 5	society of automotive engineers inc	sheet metal	Avl	RFQ
AMS-QQ-A-250 5-CDT3-0 016X12X36	society of automotive engineers inc	sheet metal	Avl	RFQ
AMS QQ A 250 5 T3 0 016X12X36	society of automotive engineers inc	sheet metal	Avl	RFQ
AMS QQ A 250 5 T3 0 016X12X36	sae inc	sheet metal	Avl	RFQ

Characteristics Data of NSN 9535015317783

MRC	Criteria	Characteristic
AARN	FABRICATION METHOD	ROLLED
ABGL	WIDTH	12.000 INCHES NOMINAL
ABRY	LENGTH	36.000 INCHES NOMINAL
ADVM	CROSS-SECTIONAL THICKNESS	0.0160 INCHES NOMINAL
AGAV	III END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
AGTA	BASIC SHAPE STYLE	SOLID
ALBY	III USAGE DESIGN	AIRCRAFT
CQBC	MINIMUM TENSILE STRENGTH	59000 POUNDS PER SQUARE INCH
CQHQ	MINIMUM YIELD STRENGTH	39000 POUNDS PER SQUARE INCH
FEAT	SPECIAL FEATURES	THIN LAYERS APPROXIMATELY EQUAL THICKNESS OF ALUMINUM ALLOY 1230 ANODIC TO 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-3 SOLUTION HEAT TREATED
MATT	MATERIAL	ALUMINUM ALLOY 2024
MDCL	MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE

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