AMS-QQ-A-250 4-CD0-0 05X6X36 by Society Of Automotive Engineers Inc with NSN 9535015317061 - Submit a Quote
Part No. : AMS-QQ-A-250 4-CD0-0 05X6X36 | Alternate P/N: AMSQQA2504CD0005X6X36 | Manufacturer : Society Of Automotive Engineers Inc | NSN : 9535-01-531-7061 |
Item Name : Sheet 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-CD0-0 05X6X36 of NSN 9535015317061 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-CD0-0 05X6X36 is a sheet 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-CD0-0 05X6X36 society of automotive engineers inc is in stock.
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Characteristics Data of NSN 9535-01-531-7061, 9535015317061MRC Criteria Characteristic MDCL Material Document And Classification QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE HEAT Heat Treatment O-ANNEALED AGTA Basic Shape Style SOLID ABRY Length 36.000 INCHES NOMINAL FEAT Special Features MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH AGAV End Item Identification FUSELAGE F4F JET AIRCRAFT MRC Decoded Requirement Clear Text Reply ABGL Width 6.000 INCHES NOMINAL ALBY Usage Design AIRCRAFT MATT Material ALUMINUM ALLOY 2024 AARN Fabrication Method ROLLED ADVM Cross-Sectional Thickness 0.0500 INCHES NOMINAL
MRC | Criteria | Characteristic |
---|---|---|
MDCL | Material Document And Classification | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |
HEAT | Heat Treatment | O-ANNEALED |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
FEAT | Special Features | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
MRC | Decoded Requirement | Clear Text Reply |
ABGL | Width | 6.000 INCHES NOMINAL |
ALBY | Usage Design | AIRCRAFT |
MATT | Material | ALUMINUM ALLOY 2024 |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0500 INCHES NOMINAL |
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