If you have been searching for AMS-QQ-A-250 5-CDT3-0 071X6X36 of Sheet Metal components with NSN 9535015317786 under FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal, look no further than Limitless Aerospace. AMS-QQ-A-250 5-CDT3-0 071X6X36 part is listed alongside the other Sheet Metal parts, and it has been manufactured by Society Of Automotive Engineers Inc (CAGE Code 81343). With current availability through our website, we invite you to request a quick and competitive quote for AMS-QQ-A-250 5-CDT3-0 071X6X36 by filling out and submitting the RFQ form below. By providing us with information such as your target price and when you need your parts by, we can ensure that we offer a personalized solution that accommodates your individual needs and requirements.
NSN parts are those that follow the NSN system as dictated by the NATO Standardization Agreements, and they contain a 13-digit serial number to optimize the procurement, stocking, and issuing of items through the federal supply system. On Limitless Aerospace, we make finding the NSN parts and components you need easy, and customers may peruse our robust NSN part catalogues or use our search engine to find specific items with ease. As the only independent distributor with a no China sourcing pledge, we choose to only stock items from top global manufacturers such as Society Of Automotive Engineers Inc. Get started on the purchasing process for AMS-QQ-A-250 5-CDT3-0 071X6X36 today and see how we can serve as your strategic sourcing partner for all of your operational needs.
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 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 | 61000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 40000 POUNDS PER SQUARE INCH |
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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 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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