L1600040-004: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 5.100 INCHES NOMINAL IN, overall_length: 5.690 INCHES NOMINAL IN, special_features: NHA L1600042; SUITABLE FOR B-1B 83-0065 THRU 86-0140 (ACFT 2 THRU 100); HEAT TREAT T7351; PLATE ALUM; DIM. ARE STOCKSIZE, aircraft_location: SUPPORT NO.1 & 2 SPOILER,WING PANEL, material_thickness: 0.560 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-533-3671, 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.
| material | ALUMINUM ALLOY 7075 |
| overall_width | 5.100 INCHES NOMINAL IN |
| overall_length | 5.690 INCHES NOMINAL IN |
| special_features | NHA L1600042; SUITABLE FOR B-1B 83-0065 THRU 86-0140 (ACFT 2 THRU 100); HEAT TREAT T7351; PLATE ALUM; DIM. ARE STOCKSIZE |
| aircraft_location | SUPPORT NO.1 & 2 SPOILER,WING PANEL |
| material_thickness | 0.560 INCHES NOMINAL IN |
| end_item_identification | B-1B |
| aircraft_mission_design_series | B-1B |
| material_document_and_classification | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-533-3671 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 5.690 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.100 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.560 INCHES NOMINAL IN |
| SPECIAL FEATURES | NHA L1600042; SUITABLE FOR B-1B 83-0065 THRU 86-0140 (ACFT 2 THRU 100); HEAT TREAT T7351; PLATE ALUM; DIM. ARE STOCKSIZE |
| AIRCRAFT LOCATION | SUPPORT NO.1 & 2 SPOILER,WING PANEL |
| END ITEM IDENTIFICATION | B-1B |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B-1B |
No substitute or cross-reference records for this part.