Aerospace Performance Parts is pleased to offer immediate purchasing options for Sae International part number AMS QQ A 250 12 CDT6 0 04X12X48, which you have taken interest in. This Sheet Metal item is listed alongside the NSN 9535-01-531-2462 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number AMS QQ A 250 12 CDT6 0 04X12X48 or any other FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal components we carry from Sae International under CAGE Code 0U583, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 9535-01-531-2462 part number AMS QQ A 250 12 CDT6 0 04X12X48 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-2462 Item PartTypeName: SHEET,METAL | 9535 | 015312462 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/12-CDT6-0,04X12X48 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CQHQ | Minimum Yield Strength | 68000 POUNDS PER SQUARE INCH |
| HEAT | Heat Treatment | T-6 SOLUTION HEAT TREATED |
| AGTA | Basic Shape Style | SOLID |
| MRC | Decoded Requirement | Clear Text Reply |
| ABRY | Length | 48.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE, F4F JET AIRCRAFT |
| CQBC | Minimum Tensile Strength | 78000 POUNDS PER SQUARE INCH |
| MATT | Material | ALUMINUM ALLOY, AMS-QQ-A-250/12, ALLOY 7075 |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
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