68A113092-2001: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.860 INCHES NOMINAL IN, overall_length: 10.150 INCHES NOMINAL IN, special_features: NHA 68A113051, aircraft_location: SUPPORT ACCESS COVER STIFFENER, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-279-9482, 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 2024 |
| overall_width | 1.860 INCHES NOMINAL IN |
| overall_length | 10.150 INCHES NOMINAL IN |
| special_features | NHA 68A113051 |
| aircraft_location | SUPPORT ACCESS COVER STIFFENER |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/5 T3 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-279-9482 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 T3 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 10.150 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.860 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | NHA 68A113051 |
| AIRCRAFT LOCATION | SUPPORT ACCESS COVER STIFFENER |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.