To receive competitive purchasing options on part number AMS QQ A 250 5 T3 0 040X6X36 by Sae International, look no further than NSN Direct. For your reference, this item has the NSN 9535-01-531-7789 and is listed with the description “Sheet Metal.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Sae International parts produced under the CAGE Code 0U583, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number AMS QQ A 250 5 T3 0 040X6X36, you can glean from the first four digits of its NSN 9535-01-531-7789 that it belongs to the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal. This being said, do not hesitate to request quotes on part number AMS QQ A 250 5 T3 0 040X6X36 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-7789 Item PartTypeName: SHEET,METAL | 9535 | 015317789 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/5-CDT3-0,04X6X36 | 5 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | Material | ALUMINUM ALLOY 2024 |
| MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
| CQHQ | Minimum Yield Strength | 39000 POUNDS PER SQUARE INCH |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 36.000 INCHES NOMINAL |
| HEAT | Heat Treatment | T-3 SOLUTION HEAT TREATED |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| ABGL | Width | 6.000 INCHES NOMINAL |
| CQBC | Minimum Tensile Strength | 59000 POUNDS PER SQUARE INCH |
| MRC | Decoded Requirement | Clear Text Reply |
| ALBY | Usage Design | AIRCRAFT |
| 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 |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
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