Part Number: AMS-QQ-A-250 5-CDT4-0 063X12X48 | Manufacturer: Society Of Automotive Engineers Inc |
NSN : 9535-01-531-7801 (9535015317801) | Item Name : sheet metal |
CAGE Code: 81343 | FSC : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
Alternate P/N : AMSQQA2505CDT40063X12X48 |
Would you like to obtain a quick quote for Society Of Automotive Engineers Inc (Cage Code 81343) Part Number AMS-QQ-A-250 5-CDT4-0 063X12X48, Sheet Metal with NSN 9535015317801? it's just a few steps away! Simply complete the form in its entirety, and we will promptly reply with a quote within 15 minutes. This is an excellent opportunity to get the quick quote for AMS-QQ-A-250 5-CDT4-0 063X12X48, so take advantage of it right away.
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MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 38000 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 SHEET THICKNESS |
HEAT | HEAT TREATMENT | T-4 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 | 0.0630 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 38000 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 SHEET THICKNESS |
HEAT | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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