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Quality guaranteed We sell only warrantied and traceable partsIf you require the NSN part AMS QQ A 250 5 CDT351 0 25X12X48, manufactured by Society Of Automotive Engineers Inc having CAGE Code 81343 and categorized under FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal under NSN 9535015317803, then look no further than NSN Gamut. Our company, which is owned and managed by ASAP Semiconductor, a distributor in the aerospace and defense industry, has an inventory of over two billion new and obsolete NSN parts, including part AMS QQ A 250 5 CDT351 0 25X12X48 Plate Metal and many more.
At NSN Gamut, we have a strict policy of not sourcing from China, ensuring that all parts you buy from us are completely traceable or sourced directly from reputable manufacturers like Society Of Automotive Engineers Inc. Obtain a quote now for AMS QQ A 250 5 CDT351 0 25X12X48. In any case if you don't find your required part submit our straight RFQ and get your part in on time.
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We offer a vast range of NSN 9535015317803 parts, including AMS QQ A 250 5 CDT351 0 25X12X48, with quick lead times and competitive prices. NSN Gamut has a large selection of in-demand parts from manufacturers such as Society Of Automotive Engineers Inc and others. To speak with a dedicated account manager, just submit an RFQ for AMS QQ A 250 5 CDT351 0 25X12X48 with your basic details like your company name parts quantity required, and get your quote in 15 minutes or less.
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.2500 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 | 62000 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 PLATE THICKNESS |
| HEAT | HEAT TREATMENT | T-351 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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