2024-T42X.032: SHEET,METAL.
The SHEET,METAL is a the manufacturer industrial component. Key specifications include width: 48.0 INCHES NOMINAL IN, length: 144.00 INCHES NOMINAL IN, material: ALUMINUM ALLOY 2024, physical_form: COIL, heat_treatment: T-42 SOLUTION HEAT TREATED, NATURAL AGED, special_features: MATERIAL IS ALUMINUM ALLOY ALCLAD 2024-T42. This part is cataloged in the U.S.
Government catalog under NSN 9535-01-697-1383, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| width | 48.0 INCHES NOMINAL IN |
| length | 144.00 INCHES NOMINAL IN |
| material | ALUMINUM ALLOY 2024 |
| physical_form | COIL |
| heat_treatment | T-42 SOLUTION HEAT TREATED, NATURAL AGED |
| special_features | MATERIAL IS ALUMINUM ALLOY ALCLAD 2024-T42 |
| end_item_identification | C-5 AIRCRAFT |
| minimum_tensile_strength | 62000 POUNDS PER SQUARE INCH LBS |
| cross-sectional_thickness | 0.032 INCHES NOMINAL IN |
| material_document_and_classification | AMS-QQ-A-250/5 AEROSPACE MATERIAL SPEC STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | METAL |
| NSN | 9535-01-697-1383 |
| LENGTH | 144.00 INCHES NOMINAL IN |
| CROSS-SECTIONAL THICKNESS | 0.032 INCHES NOMINAL IN |
| HEAT TREATMENT | T-42 SOLUTION HEAT TREATED, NATURAL AGED |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/5 AEROSPACE MATERIAL SPEC STD SINGLE MATERIAL RESPONSE |
| PHYSICAL FORM | COIL |
| SPECIAL FEATURES | MATERIAL IS ALUMINUM ALLOY ALCLAD 2024-T42 |
| MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH LBS |
| MINIMUM YIELD STRENGTH | 38000 POUNDS PER SQUARE INCH LBS |
| WIDTH | 48.0 INCHES NOMINAL IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | METAL |
No substitute or cross-reference records for this part.