NSN 9535-01-531-7800 of Plate Metal - Product Details
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Alternative NSN: 9535-01-531-7800 |
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 |
Manufacturer's List for NSN 9535-01-531-7800, 9535015317800
Part Number Related To NSN 9535-01-531-7800, 9535015317800
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
AMS-QQ-A-250-5 | 9535-01-531-7800 | plate metal | Avl | RFQ |
AMS-QQ-A-250 5-T351-1.000X6X24 | 9535-01-531-7800 | plate metal | Avl | RFQ |
AMS-QQ-A-250 5-T351-1.000X6X24 | 9535-01-531-7800 | plate metal | Avl | RFQ |
AMS-QQ-A-250 5-CDT351-1 0X6X24 | 9535-01-531-7800 | plate metal | Avl | RFQ |
AMS-QQ-A-250 5 | 9535-01-531-7800 | plate metal | Avl | RFQ |
Characteristics Data of NSN 9535015317800
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 |