Thank you for taking interest in Society Of Automotive Engineers Inc part number AMS-QQ-A-250 11-T651-0 25X12X48, which is listed with the NSN 9535-01-531-2535 and a product description of “Plate Metal.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number AMS-QQ-A-250 11-T651-0 25X12X48, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Plate Metal part with the NSN 9535-01-531-2535. For example, you can browse other Society Of Automotive Engineers Inc components that were produced under CAGE Code 81343 or listings that belong to FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number AMS-QQ-A-250 11-T651-0 25X12X48 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-2535 Item PartTypeName: PLATE,METAL | 9535 | 015312535 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/11-T651-0,25X12X48 | 5 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.2500 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE, F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 42000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 35000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, AMS-Q-250/11, ALLOY 6061 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.2500 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE, F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 42000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 35000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, AMS-Q-250/11, ALLOY 6061 |
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