68A250566-1004: FAIRING,AIRCRAFT.
The FAIRING,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, special_features: FAIRING-LOWER FORWARD,CONFORMAL FUEL TANK:RCT-7;P/N 68A250566-1003 IS THE OPPOSITE CONFIGURATION, aircraft_location: CONFORMAL FUEL TANK, material_thickness: 0.060 INCHES MINIMUM AND 0.125 INCHES MAXIMUM IN, side_for_which_designed: RIGHT SIDE, aircraft_mission_design_series: F-15I. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-441-8441, 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 |
| special_features | FAIRING-LOWER FORWARD,CONFORMAL FUEL TANK:RCT-7;P/N 68A250566-1003 IS THE OPPOSITE CONFIGURATION |
| aircraft_location | CONFORMAL FUEL TANK |
| material_thickness | 0.060 INCHES MINIMUM AND 0.125 INCHES MAXIMUM IN |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-441-8441 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.060 INCHES MINIMUM AND 0.125 INCHES MAXIMUM IN |
| SPECIAL FEATURES | FAIRING-LOWER FORWARD,CONFORMAL FUEL TANK:RCT-7;P/N 68A250566-1003 IS THE OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | CONFORMAL FUEL TANK |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
No substitute or cross-reference records for this part.