Note : We Will Not Share Your Information To Any Third Parties.
MRC | Criteria | Characteristic |
---|---|---|
ALBY | III USAGE DESIGN | AIRCRAFT |
ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 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 |
CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
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 PLATE THICKNESS |
HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
ABRY | LENGTH | 24.000 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | SOLID |
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”. |
Don’t forget That If You’d Ever Like a Quote for Parts Within 15 Minutes or Less, You Can Fill out the Instant RFQ form On this Website’S Homepage.
Request for Quote