As an ASAP Semiconductor website, you can always shop on The Distribution Pro with peace of mind, knowing that you are receiving quality-assured solutions from an NSN parts supplier you can trust. You have reached our main page for NSN 9535-01-531-7785, an item we stock that has the product description “Sheet Metal.” To help you locate and secure exactly what your projects demand, we have provided various information on NSN 9535-01-531-7785, such as the Federal Supply Group and Class associated with this NSN. Meanwhile, in-stock part numbers like AMS-QQ-A-250 5, AMS-QQ-A-250 5-CDT3-0 025X12X48, AMS-QQ-A-250 5-T3-0.025X12X48, and others are listed below, everything being available for procurement at any time. As such, be sure to request quotes on any NSN 9535-01-531-7785 listings you are interested in with the RFQ forms that are linked across the website. For us to best cater our solutions to you, please present us with as much information as you can. We always supply rapid responses to any reviewed form, and you are also welcome to call or email at any time for consultation. With how we aim to go above and beyond to bring unrivaled fulfillment solutions to the table, choose The Distribution Pro today for all your needs.
| Item Name | Sheet Metal |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
| National Item Identification Number (NIIN) | 01-531-7785 (015317785) |
| NCB Code | USA (01) |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0250 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
| HEAT | HEAT TREATMENT | T-3 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 | 0.0250 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| 9505-00-004-3522 (9505000043522) | 9505-00-006-5050 (9505000065050) | 9505-00-020-6766 (9505000206766) | 9505-00-023-0121 (9505000230121) |
| 9505-00-023-4467 (9505000234467) | 9505-00-027-2485 (9505000272485) | 9505-00-027-7789 (9505000277789) | 9505-00-035-7535 (9505000357535) |
| 9505-00-044-2161 (9505000442161) | 9505-00-051-1088 (9505000511088) | 9505-00-054-7077 (9505000547077) | 9505-00-056-1761 (9505000561761) |
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