| Mfg Part Number: AMS QQ A 250 5 | Alternate P/N: AMSQQA2505 |
| Manufacturer: Sae International | NSN : 9535-01-532-0297 |
| NIIN : 015320297 | Item Name : sheet metal |
| CAGE Code : 0U583 | 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 Sae International. 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 9535015320297. 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 Sae International. 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 |
|---|---|---|
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
| ALBY | III USAGE DESIGN | AIRCRAFT |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| 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 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 |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
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