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MRC | Criteria | Characteristic |
---|---|---|
ADVM | CROSS-SECTIONAL THICKNESS | 0.0200 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/1 |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
CQBC | MINIMUM TENSILE STRENGTH | 16000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 14000 POUNDS PER SQUARE INCH |
AARN | FABRICATION METHOD | ROLLED |
ABRY | LENGTH | 24.000 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | SOLID |
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