Thank you for your interest in Sae International part number AMS QQ A 250 5, a Sheet Metal product we carry that is featured with the NSN 9535-01-531-7789. This component is ready for purchase at any time, so you are encouraged to complete the Request for Quote (RFQ) form provided below if you would like to obtain pricing information for your consideration. All we ask is that you supply us with essential details like desired item quantities, target price, and when fulfillment is expected, as this will ensure our response caters to any distinct specifications.
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At ASAP Semiconductor, our goal is to make the process of finding and securing precise components simple, which is why we present vital listing details with each offering here on Boundless Aerospace. For instance, part number AMS QQ A 250 5 was manufactured by Sae International under the CAGECode 0U583, and with the NSN 9535-01-531-7789, it belongs to FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal. More than that, all our inventory is delivered with any pertinent qualifying certifications or manufacturer trace documentation for your further benefit. Bearing all of this in mind, be sure to request a quote for part number AMS QQ A 250 5 today, and we will be in touch as soon as possible.
| 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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