1881M72G02: NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.
NOZZLE ASSEMBLY,TURBINE,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, end_item_identification: TF39, engine_section_location: HIGH PRESSURE TURBINE, reference_data_and_literature: 2J-TF39-4, part_name_assigned_by_controlling_agency: MODULE-HIGH POWER TURBINE,ROTOR/STATOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-485-9577, 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.
| design_type | AXIAL COMPRESSOR |
| stage_number | 2 |
| end_item_identification | TF39 |
| engine_section_location | HIGH PRESSURE TURBINE |
| reference_data_and_literature | 2J-TF39-4 |
| part_name_assigned_by_controlling_agency | MODULE-HIGH POWER TURBINE,ROTOR/STATOR |
| NSN | 2840-01-485-9577 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| REFERENCE DATA AND LITERATURE | 2J-TF39-4 |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MODULE-HIGH POWER TURBINE,ROTOR/STATOR |
| END ITEM IDENTIFICATION | TF39 |
No substitute or cross-reference records for this part.