264H213005-12: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: STEEL COMP 631, thickness: 0.150 INCHES NOMINAL IN, overall_width: 2.740 INCHES NOMINAL IN, overall_length: 28.890 INCHES NOMINAL IN, aircraft_location: MID FUSELAGE UPPER LONGERON REPAIR, aircraft_mission_design_series: A-10. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-577-3559, 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 | STEEL COMP 631 |
| thickness | 0.150 INCHES NOMINAL IN |
| overall_width | 2.740 INCHES NOMINAL IN |
| overall_length | 28.890 INCHES NOMINAL IN |
| aircraft_location | MID FUSELAGE UPPER LONGERON REPAIR |
| aircraft_mission_design_series | A-10 |
| material_document_and_classification | AMS5528 ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | DOUBLER |
| NSN | 1560-01-577-3559 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5528 ASSN STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 28.890 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.740 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | MID FUSELAGE UPPER LONGERON REPAIR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER |
| MATERIAL | STEEL COMP 631 |
| AIRCRAFT MISSION DESIGN SERIES | A-10 |
| THICKNESS | 0.150 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.