MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE, F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | III USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 34000 POUNDS PER SQUARE INCH |
FEAT | SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | H-34 STRAIN HARDENED |
MATT | MATERIAL | ALUMINUM ALLOY 5052 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/8 FED SPEC 1ST MATERIAL RESPONSE |