MRC | Criteria | Characteristic |
---|---|---|
ADVM | CROSS-SECTIONAL THICKNESS | 0.0500 INCHES NOMINAL |
ALBY | III USAGE DESIGN | AIRCRAFT |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AARN | FABRICATION METHOD | ROLLED |
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; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
AGTA | BASIC SHAPE STYLE | SOLID |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
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