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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 : 9535-01-532-0308
NIIN : 015320308
CAGE Code : 0U583
Manufacturer: Sae International
Item Name : Sheet Metal
If you’re in need of NSN parts, look no further than NSN Orbit. Owned and operated by ASAP Semiconductor, we have access to an unparalleled inventory of parts and components for the aerospace, civil aviation, defense, electronics, and industrial markets. This includes parts such as Sheet Metal from Sae International, as well as part numbers like AMS-QQ-A-250 5 and many more. NSN Orbit has more than two billion new and obsolete parts readily available with short lead times and competitive prices, and as we are an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited business, and the only independent distributor with a strict No China Sourcing Pledge, each part we sell is fully traceable or comes directly from the manufacturer.
Our website offers an array of parametric search capabilities that allow our customers to search for parts through a number of filters, one of which is the National Stock Number, or NSN. A National Stock Number is an identifier applied to any item of supply that is repeatedly procured, stocked, stored, issued, and used throughout the federal supply system. NSN Orbit has a broad selection of NSN parts such as 9535015320308 from manufacturers like Sae International. To begin the purchasing process immediately, submit an RFQ today for part number AMS-QQ-A-250 5.
| MRC | Criteria | Characteristic |
|---|---|---|
| ALBY | USAGE DESIGN | AIRCRAFT |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| 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 |
| AARN | FABRICATION METHOD | ROLLED |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0500 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
 |
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