NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-531-7802 Item Description: Sheet Metal | 9535 | 015317802 | 0 | N | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS QQ A 250 5 | 5 | 1 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ALBY | III USAGE DESIGN | AIRCRAFT |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 65000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 56000 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 SHEET THICKNESS |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | SOLID |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
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