NSN 9535-01-531-7800 of Plate Metal - Parts Details
| Alternative NSN: 9535015317800 |
| 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: 015317800 |
| NCB Code: USA (01) |
| Manufacturers: Society Of Automotive Engineers Inc , Sae International |
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 5-T351-1.000X6X24, AMS-QQ-A-250 5-CDT351-1 0X6X24, AMS-QQ-A-250 5, AMS QQ A 250 5 under NSN 9535-01-531-7800 of Plate Metal manufactured by Society Of Automotive Engineers Inc, Sae International.
Federal Supply Class of NSN 9535-01-531-7800 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 9535-01-531-7800, 9535015317800
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Part No Manufacturer Item Name QTY RFQ AMS-QQ-A-250 5-T351-1.000X6X24 Society Of Automotive Engineers Inc plate metal Avl RFQ AMS-QQ-A-250 5-T351-1.000X6X24 Sae International plate metal Avl RFQ AMS-QQ-A-250 5-CDT351-1 0X6X24 Society Of Automotive Engineers Inc plate metal Avl RFQ AMS-QQ-A-250 5 Sae International plate metal Avl RFQ AMS QQ A 250 5 Society Of Automotive Engineers Inc plate metal Avl RFQ
Characteristics Data of NSN 9535015317800MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ABGL WIDTH 6.000 INCHES NOMINAL ABRY LENGTH 24.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 1.0000 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID ALBY USAGE DESIGN AIRCRAFT CQBC MINIMUM TENSILE STRENGTH 62000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 42000 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 PLATE THICKNESS HEAT HEAT TREATMENT T-351 SOLUTION HEAT TREATED MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5 AARN FABRICATION METHOD ROLLED ABGL WIDTH 6.000 INCHES NOMINAL ABRY LENGTH 24.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 1.0000 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID ALBY USAGE DESIGN AIRCRAFT CQBC MINIMUM TENSILE STRENGTH 62000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 42000 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 PLATE THICKNESS HEAT HEAT TREATMENT T-351 SOLUTION HEAT TREATED MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 24.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 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 PLATE THICKNESS |
| HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 24.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 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 PLATE THICKNESS |
| HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |