ASAP Aviation Procurement is pleased to announce that part number AMS QQ A 250 5 O 0 032X12X36 of NSN 9535-01-532-0294 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 5 O 0 032X12X36 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 5 O 0 032X12X36 Society Of Automotive Engineers Inc is in stock.
Are you interested in learning more about part number AMS QQ A 250 5 O 0 032X12X36? If so, feel free to contact us by phone at +1-714-705-4780, or by email at sales@asap-aviationprocurement.com. And if you are interested in an even faster and more convenient purchasing platform, check out the ASAP Semiconductor App from Google Play or the App Store.
MRC | Criteria | Characteristic |
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MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
HEAT | Heat Treatment | O-ANNEALED |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
ABGL | Width | 12.000 INCHES NOMINAL |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
ALBY | Usage Design | AIRCRAFT |
MRC | Decoded Requirement | Clear Text Reply |
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; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
MATT | Material | ALUMINUM ALLOY 2024 |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0320 INCHES NOMINAL |
AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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