| Mfg Part Number: AMS-QQ-A-250 5 | Alternate P/N: AMSQQA2505 |
| Manufacturer: Society Of Automotive Engineers Inc | NSN : 9535-01-531-7786 |
| NIIN : 015317786 | Item Name : sheet metal |
| CAGE Code : 81343 | FSC : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
Thank you for your interest in our available AMS-QQ-A-250 5 NSN part. This part number AMS-QQ-A-250 5 is a Sheet Metal listed under the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal, and it is manufactured by Society Of Automotive Engineers Inc. At Internet of Components, all of our stock and inventory are available for purchase today, ready to ship with short lead times and competitive pricing. Whether you are in need of parts that are new, used, or obsolete, our team of industry experts is readily available 24/7x365 to fulfill all of your operational
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Internet of Components is a premier supplier of AMS-QQ-A-250 5 NSN component, and we carry recently requested NSN components such as 9535015317786. We strive to only provide our customers with quality parts, which is why we choose to source our inventory from thousands of global manufacturers such as Society Of Automotive Engineers Inc. If you are interested in this particular item, we invite you to begin the purchasing process for AMS-QQ-A-250 5 today by filling out and submitting an Instant RFQ. Once received, a member of our staff will review and reach out to you in 15 minutes or less to provide a personalized quote that caters towards your individual needs. Get started on the purchasing process today and see how we are revolutionizing the purchasing process.
| MRC | Criteria | Characteristic |
|---|---|---|
| ALBY | III USAGE DESIGN | AIRCRAFT |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 40000 POUNDS PER SQUARE INCH |
| AARN | FABRICATION METHOD | ROLLED |
| 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 |
| AGTA | BASIC SHAPE STYLE | SOLID |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
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