Welcome to National Stock Numbers Quotes, your go-to solution for Sheet Metal components by Society Of Automotive Engineers Inc. With over 2 billion ready-to-purchase products in our inventory, customers can easily meet rigid time constraints and inflexible budget parameters. National Stock Numbers Quotes maintains a diverse database of items that suit a myriad of industry verticals, including aerospace, defense, and civil sectors, among others. On this page, you can submit a quote request for part number AMS-QQ-A-250 5-CDT81-0 063X12X48 with NSN 9535015317802 to receive a customized solution in as little as 15 minutes or less.
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At National Stock Numbers Quotes, we make it a priority to meet our customers’ operational requirements, so we keep catalogs fully stocked with in-demand NSN parts like those with the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal by Society Of Automotive Engineers Inc. For additional specification regarding your part needs, you can also find a wide range of items by their respective CAGE Code, such as 81343, and many other designations for your ease-of-search. Kick off the procurement process with a competitive quote for NSN 9535-01-531-7802 today and see why customers continuously rely on National Stock Numbers Quotes time and time again. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-7802 Item PartTypeName: SHEET,METAL | 9535 | 015317802 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/5-CDT81-0,063X12X48 | 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 | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 65000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 56000 POUNDS PER SQUARE INCH |
| 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 | T-81 SOLUTION HEAT TREATED |
| 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 | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 65000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 56000 POUNDS PER SQUARE INCH |
| 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 | T-81 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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