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Thank you for your interest in NSN part number AMS-QQ-A-250 5 under NSN 9535015317795 on Click Aerospace. Click Aerospace is a website owned and operated by ASAP Semiconductor, offering customers access to an unparalleled inventory of premium parts that cater to a variety of industries and applications. Sheet Metal is an item listed with the part number AMS-QQ-A-250 5, and FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal and it is manufactured by Sae International having CAGE Code 0U583. This item, alongside the rest of our listed NSN parts, is readily available for purchase through our website now. Get started on the purchasing process today by filling out and submitting an Instant RFQ as provided through our website. Once received, a member of our staff will reach out to you in 15 minutes or less to offer a personalized quote based on your individual needs.
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Click Aerospace is a leading independent distributor of NSN part AMS-QQ-A-250 5, and we can help you procure NSN components such as 9535015317795 and many more. The quality of our inventory is of the utmost importance to us, and thus we choose to only source our parts from global manufacturers like Sae International. Get started with a competitive quote today when you submit an Instant RFQ and experience how we are revolutionizing the parts procurement process.
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 54000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
| HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 54000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
| HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
Glad You Chose Click Aerospace as Your Parts Distributor Website today. We Hope that You Will Remember Us the Next Time You’re Looking for Required Parts.
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