NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-531-7065 Item Description: Sheet Metal | 9535 | 015317065 | 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 4-Cd0-0 09x12x48 | 5 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0900 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | III USAGE DESIGN | AIRCRAFT |
FEAT | SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |