160J612461-15: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 6.600 INCHES NOMINAL IN, overall_length: 8.100 INCHES NOMINAL IN, aircraft_location: WG OUTER PNL REPAIR-MID SPAR WEB, material_thickness: 0.063 INCHES NOMINAL IN, aircraft_station_number: WS110.0 TO WS143.0. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-490-0709, 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 | 6.600 INCHES NOMINAL IN |
| overall_length | 8.100 INCHES NOMINAL IN |
| special_features | HEAT TREAT T-6; SHEET,BARE; DIMENSIONS ARE STOCKSIZE; NHA -2; MANF. SUGGESTED NAME(A-10A WG OUTER PANEL REPAIR-MID SPAR WEB) A |
| aircraft_location | WG OUTER PNL REPAIR-MID SPAR WEB |
| material_thickness | 0.063 INCHES NOMINAL IN |
| aircraft_station_number | WS110.0 TO WS143.0 |
| aircraft_mission_design_series | A-10A A |
| material_document_and_classification | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-490-0709 |
| AIRCRAFT STATION NUMBER | WS110.0 TO WS143.0 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 8.100 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.600 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT T-6; SHEET,BARE; DIMENSIONS ARE STOCKSIZE; NHA -2; MANF. SUGGESTED NAME(A-10A WG OUTER PANEL REPAIR-MID SPAR WEB) A |
| AIRCRAFT LOCATION | WG OUTER PNL REPAIR-MID SPAR WEB |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | A-10A A |
No substitute or cross-reference records for this part.