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 AMS-QQ-A-250 4-CDT3-0 1X12X48, a Society Of Automotive Engineers Inc item with the NSN 9535015316271 that is listed alongside the description “Sheet Metal.” If you are interested in part number AMS-QQ-A-250 4-CDT3-0 1X12X48 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 AMS-QQ-A-250 4-CDT3-0 1X12X48 is specifically listed with the NSN 9535-01-531-6271, 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 |
|---|---|---|---|---|---|---|
| 9535-01-531-6271 Item PartTypeName: SHEET,METAL | 9535 | 015316271 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/4-CDT3-0,1X12X48 | 5 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | Material | ALUMINUM ALLOY 2024 |
| HEAT | Heat Treatment | T-3 SOLUTION HEAT TREATED |
| CQHQ | Minimum Yield Strength | 42000 POUNDS PER SQUARE INCH |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 48.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| CQBC | Minimum Tensile Strength | 63000 POUNDS PER SQUARE INCH |
| MDCL | Material Document And Classification | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |
| ALBY | Usage Design | AIRCRAFT |
| AARN | Fabrication Method | ROLLED |
| MRC | Decoded Requirement | Clear Text Reply |
| ADVM | Cross-Sectional Thickness | 0.1000 INCHES NOMINAL |
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