To receive competitive purchasing options on part number AMS-QQ-A-250 5 by Society Of Automotive Engineers Inc, look no further than NSN Direct. For your reference, this item has the NSN 9535-01-532-0311 and is listed with the description “Sheet Metal.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Society Of Automotive Engineers Inc parts produced under the CAGE Code 81343, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number AMS-QQ-A-250 5, you can glean from the first four digits of its NSN 9535-01-532-0311 that it belongs to the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal. This being said, do not hesitate to request quotes on part number AMS-QQ-A-250 5 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-532-0311 Item PartTypeName: SHEET,METAL | 9535 | 015320311 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/5-CD0-0,125X12X48 | 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 | 0.1250 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| FEAT | SPECIAL FEATURES | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS; |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.1250 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| FEAT | SPECIAL FEATURES | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS; |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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