68A111211-2019: RIB,AIRFOIL.
The RIB,AIRFOIL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 8.860 INCHES NOMINAL IN, overall_length: 15.500 INCHES NOMINAL IN, special_features: USEABLE ON F-15E CUM-163;DIM AND TOLERANCING BASED ON ANSI Y14.5-1966, aircraft_location: WING LEADING EDGE, material_thickness: 0.063 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-487-7326, 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 | 8.860 INCHES NOMINAL IN |
| overall_length | 15.500 INCHES NOMINAL IN |
| special_features | USEABLE ON F-15E CUM-163;DIM AND TOLERANCING BASED ON ANSI Y14.5-1966 |
| aircraft_location | WING LEADING EDGE |
| material_thickness | 0.063 INCHES NOMINAL IN |
| aircraft_station_number | XFS140.396 |
| aircraft_mission_design_series | F-15E |
| material_document_and_classification | QQ-A-250/4 COND-O FED SPEC 1ST MATERIAL RESPONSE |
| NSN | 1560-01-487-7326 |
| AIRCRAFT STATION NUMBER | XFS140.396 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 COND-O FED SPEC 1ST MATERIAL RESPONSE |
| OVERALL LENGTH | 15.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 8.860 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| SPECIAL FEATURES | USEABLE ON F-15E CUM-163;DIM AND TOLERANCING BASED ON ANSI Y14.5-1966 |
| AIRCRAFT LOCATION | WING LEADING EDGE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15E |
No substitute or cross-reference records for this part.