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AMS QQ A 250 4 CDT3 0 19X12X48 by Society Of Automotive Engineers Inc – NSN 9535015316273 Available for Quote

Thank you for taking interest in Society Of Automotive Engineers Inc part number AMS QQ A 250 4 CDT3 0 19X12X48, which is listed with the NSN 9535015316273 and a product description of “Sheet Metal.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.

Alongside part number AMS QQ A 250 4 CDT3 0 19X12X48, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Sheet Metal part with the NSN 9535015316273. For example, you can browse other Society Of Automotive Engineers Inc components that were produced under CAGE Code or listings that belong to FSC with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number AMS QQ A 250 4 CDT3 0 19X12X48 and other desired offerings on Aerospace Spare.

Specifications

Part NumberAMS QQ A 250 4 CDT3 0 19X12X48
DescriptionSheet Metal
ManufacturerSociety Of Automotiv
NSN9535-01-531-6273(9535015316273)
Item NameSheet Metal
CAGE Code81343
NIIN01-531-6273(015316273)
FSC Code9535 Plate Sheet Strip and Foil Nonferrous Base Metal
FSG Code95 Metal Bars, Sheets, and Shapes
SKUams-qq-a-250-4-cdt3-0-19x12x48
NCB Code01
CountryUSA

Description

Sheet Metal

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Characteristics Data of NSN 9535-01-531-6273, 9535015316273

MRCCriteriaCharacteristic
ALBYIII USAGE DESIGNAIRCRAFT
ADVMCROSS-SECTIONAL THICKNESS0.1900 INCHES NOMINAL
MATLMATERIALALUMINUM ALLOY, QQ-A-250/4
AGAVIII END ITEM IDENTIFICATIONFUSELAGE F4F JET AIRCRAFT
CQBCMINIMUM TENSILE STRENGTH64000 POUNDS PER SQUARE INCH
CQHQMINIMUM YIELD STRENGTH42000 POUNDS PER SQUARE INCH
AARNFABRICATION METHODROLLED
ABGLWIDTH12.000 INCHES NOMINAL
HEATHEAT TREATMENTT-3 SOLUTION HEAT TREATED
ABRYLENGTH48.000 INCHES NOMINAL
AGTABASIC SHAPE STYLESOLID