AMS-QQA250-15: SHEET,METAL.
The SHEET,METAL is a the manufacturer industrial component. Key specifications include width: 12.000 INCHES NOMINAL IN, length: 48.000 INCHES NOMINAL IN, material: ALUMINUM ALLOY 7178, basic_shape_style: SOLID, fabrication_method: ROLLED, end_item_identification: FIXED WING AIRCRAFT, MCDONNEL DOUGLAS F-4F PHANTOM. This part is cataloged in the U.S.
Government catalog under NSN 9535-00-555-4931, 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 | 12.000 INCHES NOMINAL IN |
| length | 48.000 INCHES NOMINAL IN |
| material | ALUMINUM ALLOY 7178 |
| basic_shape_style | SOLID |
| fabrication_method | ROLLED |
| end_item_identification | FIXED WING AIRCRAFT, MCDONNEL DOUGLAS F-4F PHANTOM |
| minimum_tensile_strength | 38000 POUNDS PER SQUARE INCH LBS |
| cross-sectional_thickness | 0.063 INCHES NOMINAL IN |
| material_document_and_classification | QQ-A-250/14 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 9535-00-555-4931 |
| LENGTH | 12.000 FEET NOMINAL FT |
| CLADDING THICKNESS | 0.0023 INCHES OVERALL IN |
| CROSS-SECTIONAL THICKNESS | 0.090 INCHES NOMINAL IN |
| HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/15 FED SPEC 1ST MATERIAL RESPONSE |
| BASIC SHAPE STYLE | SOLID |
| WEIGHT PER UNIT MEASURE | 1.326 POUNDS PER SQUARE FOOT LBS |
| NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| MINIMUM TENSILE STRENGTH | 80000 POUNDS PER SQUARE INCH LBS |
| MINIMUM YIELD STRENGTH | 70000 POUNDS PER SQUARE INCH LBS |