Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number QQ A 250 11 T651 0 375X8X36, a Society Of Automotive Engineers Inc item with the NSN 9535015312534 that is listed alongside the description “Plate Metal.” If you are interested in part number QQ A 250 11 T651 0 375X8X36 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number QQ A 250 11 T651 0 375X8X36 is specifically listed with the NSN 9535-01-531-2534, and this code can be used to determine that it falls under FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal. Additionally, while tracing back to Society Of Automotive Engineers Inc, this NSN part was specifically produced under CAGE Code 81343. With our services and dedication to simple procurement in mind, get started with us today!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-2534 Item PartTypeName: PLATE,METAL | 9535 | 015312534 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/11-CT651-0,375X8X36 | 5 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 8.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.3750 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 | 8.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.3750 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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