68R092051-2015: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.150 INCHES NOMINAL IN, overall_length: 9.120 INCHES NOMINAL IN, special_features: REQUESTEDNAME:FILLER;P/N 68R092051-2016 IS THE OPPOSITE CONFIGURATION, aircraft_location: SKIN REPAIR-WING INBOARD TORQUE BOX UPPER AFT, material_thickness: 0.040 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-441-4133, 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 | 1.150 INCHES NOMINAL IN |
| overall_length | 9.120 INCHES NOMINAL IN |
| special_features | REQUESTEDNAME:FILLER;P/N 68R092051-2016 IS THE OPPOSITE CONFIGURATION |
| aircraft_location | SKIN REPAIR-WING INBOARD TORQUE BOX UPPER AFT |
| material_thickness | 0.040 INCHES NOMINAL IN |
| aircraft_station_number | XW155.024 |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/12,-T6 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-441-4133 |
| AIRCRAFT STATION NUMBER | XW155.024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12,-T6 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 9.120 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.150 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | REQUESTEDNAME:FILLER;P/N 68R092051-2016 IS THE OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | SKIN REPAIR-WING INBOARD TORQUE BOX UPPER AFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.