We appreciate your interest in Society Of Automotive Engineers Inc part number AMS-QQ-A-250 4-CD0-0 04X12X48, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number AMS-QQ-A-250 4-CD0-0 04X12X48 is listed with the NSN 9535-01-531-7063 and description “Sheet Metal.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Society Of Automotive Engineers Inc under the CAGE Code 81343 or that similarly fall under the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 9535-01-531-7063 parts and Sheet Metal items your operations require, so request a quote today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-7063 Item PartTypeName: SHEET,METAL | 9535 | 015317063 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/4-O-0.040X12X48 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
| MDCL | Material Document And Classification | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |
| HEAT | Heat Treatment | O-ANNEALED |
| AGTA | Basic Shape Style | SOLID |
| FEAT | Special Features | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH |
| ABRY | Length | 48.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| ALBY | Usage Design | AIRCRAFT |
| MATT | Material | ALUMINUM ALLOY 2024 |
| AARN | Fabrication Method | ROLLED |
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