AMS-QQ-A-250 4-CDT351-0 375X6X36 by Society Of Automotive Engineers Inc with NSN 9535015316280 - Submit a Quote
Part No. : AMS-QQ-A-250 4-CDT351-0 375X6X36 | Alternate P/N: AMSQQA2504CDT3510375X6X36 | Manufacturer : Society Of Automotive Engineers Inc | NSN : 9535-01-531-6280 |
Item Name : Plate Metal | CAGE Code : 81343 | FSC : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
ASAP Aviation Procurement is pleased to announce that part number AMS-QQ-A-250 4-CDT351-0 375X6X36 of NSN 9535015316280 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number AMS-QQ-A-250 4-CDT351-0 375X6X36 is a plate metal manufactured by society of automotive engineers inc under CAGE Code 81343. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote.In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA. AMS-QQ-A-250 4-CDT351-0 375X6X36 society of automotive engineers inc is in stock.
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Characteristics Data of NSN 9535-01-531-6280, 9535015316280MRC Criteria Characteristic MATT Material ALUMINUM ALLOY 2024 HEAT Heat Treatment T-351 SOLUTION HEAT TREATED CQHQ Minimum Yield Strength 42000 POUNDS PER SQUARE INCH AGTA Basic Shape Style SOLID ABRY Length 36.000 INCHES NOMINAL AGAV End Item Identification FUSELAGE F4F JET AIRCRAFT CQBC Minimum Tensile Strength 64000 POUNDS PER SQUARE INCH ABGL Width 6.000 INCHES NOMINAL MDCL Material Document And Classification QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE ALBY Usage Design AIRCRAFT AARN Fabrication Method ROLLED MRC Decoded Requirement Clear Text Reply ADVM Cross-Sectional Thickness 0.3750 INCHES NOMINAL
MRC | Criteria | Characteristic |
---|---|---|
MATT | Material | ALUMINUM ALLOY 2024 |
HEAT | Heat Treatment | T-351 SOLUTION HEAT TREATED |
CQHQ | Minimum Yield Strength | 42000 POUNDS PER SQUARE INCH |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
CQBC | Minimum Tensile Strength | 64000 POUNDS PER SQUARE INCH |
ABGL | Width | 6.000 INCHES NOMINAL |
MDCL | Material Document And Classification | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |
ALBY | Usage Design | AIRCRAFT |
AARN | Fabrication Method | ROLLED |
MRC | Decoded Requirement | Clear Text Reply |
ADVM | Cross-Sectional Thickness | 0.3750 INCHES NOMINAL |
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