68A332222-2002: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_width: 18.000 INCHES NOMINAL IN, overall_length: 36.000 INCHES NOMINAL IN, special_features: MATERIAL:6AL-4V;P/N 68A332222-2001 IS THE OPPOSITE CONFIGURATION V, aircraft_location: EMPENNAGE SUPPORT BEAM, material_thickness: 4.000 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-448-9822, 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 | 18.000 INCHES NOMINAL IN |
| overall_length | 36.000 INCHES NOMINAL IN |
| special_features | MATERIAL:6AL-4V;P/N 68A332222-2001 IS THE OPPOSITE CONFIGURATION V |
| aircraft_location | EMPENNAGE SUPPORT BEAM |
| material_thickness | 4.000 INCHES NOMINAL IN |
| aircraft_station_number | FS815.000 |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | MIL-T-9046,AB-1,CONDITION ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-448-9822 |
| AIRCRAFT STATION NUMBER | FS815.000 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046,AB-1,CONDITION ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 36.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 18.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 4.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATERIAL:6AL-4V;P/N 68A332222-2001 IS THE OPPOSITE CONFIGURATION V |
| AIRCRAFT LOCATION | EMPENNAGE SUPPORT BEAM |
| MATERIAL | TITANIUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
No substitute or cross-reference records for this part.