MRC | Criteria | Characteristic |
---|---|---|
ALBY | III USAGE DESIGN | AIRCRAFT |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0800 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS; MAXIMUM TENSILE STRENGTH 32000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | O-ANNEALED |
AGTA | BASIC SHAPE STYLE | SOLID |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
If You’d Like to Stay Up to Date On Our Latest, Up-To-Date NSN Parts; Kindly Explore Our Catalog and Get Quote for Your Required Part Number.
Request for Quote