| Alternative NSN: 9535-01-531-7140 |
| Item Name: Plate Metal |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
| NIIN: 015317140 |
| NCB Code: USA (01) |
| Manufacturers: Sae International , Society Of Automotive Engineers Inc |
Veritable Aviation, owned and operated by ASAP Semiconductor, makes the parts procurement process for NSN 9535-01-531-7140 as streamlined as possible. Our easy to use search engine opens up our 6-billion-part inventory open to our loyal customers. Simply type in a part number such as AMS-QQ-A-250 4, AMS-QQ-A-250 4-CD351-0 250X48X12, AMS-QQ-A-250 4-T351-0.250X48X12, AMS-QQ-A-250-4-T351-0.250X48X12 or NSN 9535-01-531-7140 and receive a quote within fifteen minutes or less from one of our dedicated account managers. We work with well-known industry names Sae International, Society Of Automotive Engineers Inc.
We are dedicated to providing only the best products under NSN 9535-01-531-7140 through our quality assurance practices, earning us our FAA-AC 0056B accreditation and ISO 9001:2015 certification. To get your parts procurement process started, fill out the request for quote form below.
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 4 | Sae International | plate metal | Avl | RFQ |
| AMS-QQ-A-250 4 | Society Of Automotive Engineers Inc | plate metal | Avl | RFQ |
| AMS-QQ-A-250 4-CD351-0 250X48X12 | Society Of Automotive Engineers Inc | plate metal | Avl | RFQ |
| AMS-QQ-A-250 4-T351-0.250X48X12 | Sae International | plate metal | Avl | RFQ |
| AMS-QQ-A-250-4-T351-0.250X48X12 | Society Of Automotive Engineers Inc | plate metal | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.2500 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 64000 POUNDS PER SQUARE INCH |
| HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
| AARN | FABRICATION METHOD | ROLLED |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4 |
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9505-00-035-7535 (9505000357535) |
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9505-00-051-1088 (9505000511088) |
9505-00-054-7077 (9505000547077) |
9505-00-056-1761 (9505000561761) |
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