We appreciate your interest in part number AMS-QQ-A-250 4-CDT3-0 05X48X12, which is currently available for purchase here on Jet Force Aero. For your reference, this item is produced by Society Of Automotive Engineers Inc and is listed with the NSN 9535-01-531-5841, as well as the description “Sheet Metal.” If this matches your requirements, we encourage you to fill out the Request for Quote (RFQ) form featured on this page to receive tailored purchasing options on part number AMS-QQ-A-250 4-CDT3-0 05X48X12. All that we ask is that you submit as many details about your procurement needs as possible, such as your desired quantity, budget, and anticipated fulfillment timeframe, as this will enable our specialists to craft an ideal response for you.
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In addition to part number AMS-QQ-A-250 4-CDT3-0 05X48X12, be sure to explore our website further for related items produced by Society Of Automotive Engineers Inc under the CAGE Code 81343 as you wish. We also feature catalogs to help you find additional options that are categorized under FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal and the NSN 9535-01-531-5841. Regardless of which NSN parts you need from us, rest assured that we will always treat you to affordable solutions where you never have to sacrifice quality or prompt fulfillment. We are ready to assist you with all your sourcing needs, so kick off quotation at your convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-5841 Item PartTypeName: SHEET,METAL | 9535 | 015315841 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/4-CDT3-0,05X48X12 | 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 | 0.0500 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | III USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 63000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |
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