160D612301-28: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 12.500 INCHES NOMINAL IN, aircraft_location: SPAR INSTALLATION,OUTBOARD WING PANEL, material_thickness: 0.094 INCHES NOMINAL IN, aircraft_station_number: WS110.0 TO WS331.84, aircraft_mission_design_series: A-10. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-147-4587, 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_length | 12.500 INCHES NOMINAL IN |
| aircraft_location | SPAR INSTALLATION,OUTBOARD WING PANEL |
| material_thickness | 0.094 INCHES NOMINAL IN |
| aircraft_station_number | WS110.0 TO WS331.84 |
| aircraft_mission_design_series | A-10 |
| material_document_and_classification | QQ-A-200/11 T6511 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-147-4587 |
| AIRCRAFT STATION NUMBER | WS110.0 TO WS331.84 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 T6511 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 12.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.094 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | SPAR INSTALLATION,OUTBOARD WING PANEL |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | A-10 |
No substitute or cross-reference records for this part.