68A250184-2017: SKIN,AIRCRAFT.
The SKIN,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, thickness: 0.100 INCHES NOMINAL IN, overall_width: 13.600 INCHES NOMINAL IN, overall_length: 33.900 INCHES NOMINAL IN, aircraft_location: CONFORMAL FUEL TANK,LCT-6 CUMULATIVE 25 AND UP, aircraft_station_number: FS415 TO FS428.390. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-448-0655, 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 |
| thickness | 0.100 INCHES NOMINAL IN |
| overall_width | 13.600 INCHES NOMINAL IN |
| overall_length | 33.900 INCHES NOMINAL IN |
| special_features | BASIC MATERIAL 7075-0 ALCLAD HEAT TREATED TO T76 PER PS15552 WITH CHEMICAL CONVERSION COAT;P/N 68A250184-2018 IS THE OPPOSITE CONFIGURATION |
| aircraft_location | CONFORMAL FUEL TANK,LCT-6 CUMULATIVE 25 AND UP |
| aircraft_station_number | FS415 TO FS428.390 |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | QQ-A-250/13,T76 FED SPEC SINGLE MATERIAL RESPONSE |
| surface_treatment_document_and_classification | PS13209 MFR REF SINGLE TREATMENT RESPONSE |
| NSN | 1560-01-448-0655 |
| AIRCRAFT STATION NUMBER | FS415 TO FS428.390 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | PS13209 MFR REF SINGLE TREATMENT RESPONSE |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13,T76 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 33.900 INCHES NOMINAL IN |
| OVERALL WIDTH | 13.600 INCHES NOMINAL IN |
| SPECIAL FEATURES | BASIC MATERIAL 7075-0 ALCLAD HEAT TREATED TO T76 PER PS15552 WITH CHEMICAL CONVERSION COAT;P/N 68A250184-2018 IS THE OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | CONFORMAL FUEL TANK,LCT-6 CUMULATIVE 25 AND UP |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
| THICKNESS | 0.100 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.