68A250714-1006: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7050, overall_length: 33.820 INCHES NOMINAL IN, special_features: U/O CONFORMAL FUEL TANK RCT-6 AND RCT-8 CUMULATIVE 1-UP;P/N 68A250714-1005 IS THE OPPOSITE CONFIGURATION, aircraft_location: CONFORMAL FUEL TANK, aircraft_station_number: FS699.870, aircraft_mission_design_series: F-15I. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-441-3134, 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 7050 |
| overall_length | 33.820 INCHES NOMINAL IN |
| special_features | U/O CONFORMAL FUEL TANK RCT-6 AND RCT-8 CUMULATIVE 1-UP;P/N 68A250714-1005 IS THE OPPOSITE CONFIGURATION |
| aircraft_location | CONFORMAL FUEL TANK |
| aircraft_station_number | FS699.870 |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | MMS 146,T7452 MFR REF SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-441-3134 |
| AIRCRAFT STATION NUMBER | FS699.870 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS 146,T7452 MFR REF SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 33.820 INCHES NOMINAL IN |
| SPECIAL FEATURES | U/O CONFORMAL FUEL TANK RCT-6 AND RCT-8 CUMULATIVE 1-UP;P/N 68A250714-1005 IS THE OPPOSITE CONFIGURATION |
| AIRCRAFT LOCATION | CONFORMAL FUEL TANK |
| MATERIAL | ALUMINUM ALLOY 7050 |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
No substitute or cross-reference records for this part.