Part Number: AMS-QQ-A-250 5 | Manufacturer: Society Of Automotive Engineers Inc | NSN: 9535-01-531-7789 (9535015317789) | Item Name : sheet metal | CAGE Code: 81343 | FSC: 9535 Plate Sheet Strip and Foil Nonferrous Base Metal | Alternate P/N : AMSQQA2505 |
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MRC | Criteria | Characteristic |
---|---|---|
MATT | Material | ALUMINUM ALLOY 2024 |
MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
CQHQ | Minimum Yield Strength | 39000 POUNDS PER SQUARE INCH |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
HEAT | Heat Treatment | T-3 SOLUTION HEAT TREATED |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
ABGL | Width | 6.000 INCHES NOMINAL |
CQBC | Minimum Tensile Strength | 59000 POUNDS PER SQUARE INCH |
MRC | Decoded Requirement | Clear Text Reply |
ALBY | Usage Design | AIRCRAFT |
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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
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