MRC | Criteria | Characteristic |
---|---|---|
ADVM | CROSS-SECTIONAL THICKNESS | 0.0200 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-250/12, ALLOY 7075 |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE, F4F JET AIRCRAFT |
ABGL | WIDTH | 8.000 INCHES NOMINAL |
CQBC | MINIMUM TENSILE STRENGTH | 76000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 67000 POUNDS PER SQUARE INCH |
AARN | FABRICATION METHOD | ROLLED |
HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | SOLID |
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