68A336201-2049: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_width: 36.690 INCHES NOMINAL IN, overall_length: 62.510 INCHES NOMINAL IN, special_features: MATERIAL:6AL-4V;P/N 68A336201-2050 IS THE OPPOSITE CONFIGURATION;USED ON NEXT HIGHER ASSEMBLY P/N 68A336201-1007 V, aircraft_location: UPPER-AFT FUSELAGE, aircraft_station_number: FS712.310 TO FS749.000. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-441-2102, 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 | TITANIUM ALLOY |
| overall_width | 36.690 INCHES NOMINAL IN |
| overall_length | 62.510 INCHES NOMINAL IN |
| special_features | MATERIAL:6AL-4V;P/N 68A336201-2050 IS THE OPPOSITE CONFIGURATION;USED ON NEXT HIGHER ASSEMBLY P/N 68A336201-1007 V |
| aircraft_location | UPPER-AFT FUSELAGE |
| aircraft_station_number | FS712.310 TO FS749.000 |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | MIL-T-9046 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-441-2102 |
| AIRCRAFT STATION NUMBER | FS712.310 TO FS749.000 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 62.510 INCHES NOMINAL IN |
| OVERALL WIDTH | 36.690 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATERIAL:6AL-4V;P/N 68A336201-2050 IS THE OPPOSITE CONFIGURATION;USED ON NEXT HIGHER ASSEMBLY P/N 68A336201-1007 V |
| AIRCRAFT LOCATION | UPPER-AFT FUSELAGE |
| MATERIAL | TITANIUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
No substitute or cross-reference records for this part.