MRC | Criteria | Characteristic |
---|---|---|
ALBY | III USAGE DESIGN | AIRCRAFT |
ADVM | CROSS-SECTIONAL THICKNESS | 0.1250 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4 |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 63000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | SOLID |
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