NSN 9535-01-531-6280 of Plate Metal - Parts Details
| Alternative NSN: 9535015316280 |
| 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: 015316280 |
| NCB Code: USA (01) |
| Manufacturers: Sae International , Society Of Automotive Engineers Inc |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers AMS-QQ-A-250 4-T351-0.375X6X36, AMS-QQ-A-250 4-CDT351-0 375X6X36, AMS-QQ-A-250 4, AMS QQ A 250 4 under NSN 9535-01-531-6280 of Plate Metal manufactured by Sae International, Society Of Automotive Engineers Inc.
Federal Supply Class of NSN 9535-01-531-6280 is FSC 9535 contains part details of Plate Sheet Strip and Foil Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9535-01-531-6280, 9535015316280
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Part No Manufacturer Item Name QTY RFQ AMS-QQ-A-250 4-T351-0.375X6X36 Sae International plate metal Avl RFQ AMS-QQ-A-250 4-T351-0.375X6X36 Society Of Automotive Engineers Inc plate metal Avl RFQ AMS-QQ-A-250 4-CDT351-0 375X6X36 Society Of Automotive Engineers Inc plate metal Avl RFQ AMS-QQ-A-250 4 Society Of Automotive Engineers Inc plate metal Avl RFQ AMS QQ A 250 4 Sae International plate metal Avl RFQ
Characteristics Data of NSN 9535015316280MRC Criteria Characteristic MATT Material ALUMINUM ALLOY 2024 HEAT Heat Treatment T-351 SOLUTION HEAT TREATED CQHQ Minimum Yield Strength 42000 POUNDS PER SQUARE INCH AGTA Basic Shape Style SOLID ABRY Length 36.000 INCHES NOMINAL AGAV End Item Identification FUSELAGE F4F JET AIRCRAFT CQBC Minimum Tensile Strength 64000 POUNDS PER SQUARE INCH ABGL Width 6.000 INCHES NOMINAL MDCL Material Document And Classification QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE ALBY Usage Design AIRCRAFT AARN Fabrication Method ROLLED MRC Decoded Requirement Clear Text Reply ADVM Cross-Sectional Thickness 0.3750 INCHES NOMINAL
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | Material | ALUMINUM ALLOY 2024 |
| HEAT | Heat Treatment | T-351 SOLUTION HEAT TREATED |
| CQHQ | Minimum Yield Strength | 42000 POUNDS PER SQUARE INCH |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 36.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| CQBC | Minimum Tensile Strength | 64000 POUNDS PER SQUARE INCH |
| ABGL | Width | 6.000 INCHES NOMINAL |
| MDCL | Material Document And Classification | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |
| ALBY | Usage Design | AIRCRAFT |
| AARN | Fabrication Method | ROLLED |
| MRC | Decoded Requirement | Clear Text Reply |
| ADVM | Cross-Sectional Thickness | 0.3750 INCHES NOMINAL |