68R092051-2007: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.560 INCHES NOMINAL IN, overall_length: 7.310 INCHES NOMINAL IN, special_features: REQUESTEDNAME:FILLER;P/N 68R092051-2008 IS THE OPPOSITE CINFIGURATION, aircraft_location: SKIN REPAIR-WING INBOARD TORQUE BOX UPPER AFT, material_thickness: 0.180 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-441-4131, 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 | 1.560 INCHES NOMINAL IN |
| overall_length | 7.310 INCHES NOMINAL IN |
| special_features | REQUESTEDNAME:FILLER;P/N 68R092051-2008 IS THE OPPOSITE CINFIGURATION |
| aircraft_location | SKIN REPAIR-WING INBOARD TORQUE BOX UPPER AFT |
| material_thickness | 0.180 INCHES NOMINAL IN |
| aircraft_station_number | XW155.024 |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/24,-T76 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-441-4131 |
| AIRCRAFT STATION NUMBER | XW155.024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/24,-T76 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 7.310 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.560 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.180 INCHES NOMINAL IN |
| SPECIAL FEATURES | REQUESTEDNAME:FILLER;P/N 68R092051-2008 IS THE OPPOSITE CINFIGURATION |
| 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.