25-2358-3: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 5.400 INCHES NOMINAL IN, overall_length: 17.900 INCHES NOMINAL IN, special_features: USED AS WEB,FWD, aircraft_location: FRONT SPAR ASSY,OUTBOARD STRUT, material_thickness: 0.063 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-159-9650, 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 | 5.400 INCHES NOMINAL IN |
| overall_length | 17.900 INCHES NOMINAL IN |
| special_features | USED AS WEB,FWD |
| aircraft_location | FRONT SPAR ASSY,OUTBOARD STRUT |
| material_thickness | 0.063 INCHES NOMINAL IN |
| aircraft_mission_design_series | B-52 |
| material_document_and_classification | QQ-A-287 T6 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-159-9650 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-287 T6 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 17.900 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.400 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| SPECIAL FEATURES | USED AS WEB,FWD |
| AIRCRAFT LOCATION | FRONT SPAR ASSY,OUTBOARD STRUT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B-52 |
No substitute or cross-reference records for this part.