MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.1900 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE, F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
CQBC | MINIMUM TENSILE STRENGTH | 78000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 69000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-250/12, ALLOY 7075 |