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Quality guaranteed We sell only warrantied and traceable partsMfg Part Number: AMS-QQ-A-250 5
Alternate P/N: AMSQQA2505
NSN : 9535-01-532-0298
NIIN : 015320298
CAGE Code : 0U583
Manufacturer: Sae International
Item Name : Sheet Metal
In our inventory, we have more than two billion new and obsolete NSN part like AMS-QQ-A-250 5. Aviation Sphere can offer an impressive selection of NSN parts. This includes parts like AMS-QQ-A-250 5 Sheet Metal from manufacturer Sae International and many more, all of which are available with short lead times and competitive prices. For parts not in our inventory, our dedicated account managers can help you track them down through our international supply chain network that extends across the United States, Canada, and the United Kingdom. Furthermore, Aviation Sphere is an AS9120B, ISO 9001:2015, and FAA AC 0056B accredited business, as well as the only independent distributor with a strict No China Sourcing Pledge, allowing us to ensure that each part part like AMS-QQ-A-250 5, you purchase from us is fully traceable or comes directly from its manufacturer.
Our website offers a number of parametric search capabilities, one of which allows you to search specifically for NSN part like AMS-QQ-A-250 5. This means you can quickly sort through National Stock Numbers such as 9535015320298 and find parts from quality manufacturers like Sae International and many others. To begin the purchasing process immediately, submit an RFQ today. Our team of dedicated account managers is standing by and will respond to all inquiries in 15 minutes or less.
| MRC | Criteria | Characteristic |
|---|---|---|
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 INCHES NOMINAL |
| ALBY | III USAGE DESIGN | AIRCRAFT |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| 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 |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
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