68G250001-1001: TANK,FUEL,AIRCRAFT.
The TANK,FUEL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY AND PLASTIC AND STEEL AND TITANIUM ALLOY, overall_width: 35.000 INCHES NOMINAL IN, overall_height: 56.000 INCHES NOMINAL IN, overall_length: 390.000 INCHES NOMINAL IN, special_features: MODIFICATION OF 68A250001-1021 PER TO 6J14-5-11-521 TO ADD EJECTOR PUMP;P/N 68G250001-1002 IS THE OPPOSITE CONFIGURATION, aircraft_location: CONFORMAL FUEL TANK. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-446-5806, 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 AND PLASTIC AND STEEL AND TITANIUM ALLOY |
| overall_width | 35.000 INCHES NOMINAL IN |
| overall_height | 56.000 INCHES NOMINAL IN |
| overall_length | 390.000 INCHES NOMINAL IN |
| special_features | MODIFICATION OF 68A250001-1021 PER TO 6J14-5-11-521 TO ADD EJECTOR PUMP;P/N 68G250001-1002 IS THE OPPOSITE CONFIGURATION |
| aircraft_location | CONFORMAL FUEL TANK |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | F-15E |
| NSN | 1560-01-446-5806 |
| OVERALL HEIGHT | 56.000 INCHES NOMINAL IN |
| OVERALL LENGTH | 390.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 35.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | MODIFICATION OF 68A250001-1021 PER TO 6J14-5-11-521 TO ADD EJECTOR PUMP;P/N 68G250001-1002 IS THE OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | CONFORMAL FUEL TANK |
| MATERIAL | ALUMINUM ALLOY AND PLASTIC AND STEEL AND TITANIUM ALLOY |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-15E |
No substitute or cross-reference records for this part.