9547M26G07: NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.
NOZZLE ASSEMBLY,TURBINE,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 31.500 INCHES NOMINAL IN, end_item_identification: ACFT ENG F110GE129, engine_section_location: HIGH PRESSURE TURBINE, criticality_code_justification: AGAV, part_name_assigned_by_controlling_agency: NOZZLE ASSEMBLY,HIGH PRESSURE TURBINE STATOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-447-2847, 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 |
| overall_length | 31.500 INCHES NOMINAL IN |
| end_item_identification | ACFT ENG F110GE129 |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | NOZZLE ASSEMBLY,HIGH PRESSURE TURBINE STATOR |
| NSN | 2840-01-447-2847 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 31.500 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE ASSEMBLY,HIGH PRESSURE TURBINE STATOR |
| END ITEM IDENTIFICATION | ACFT ENG F110GE129 |
No substitute or cross-reference records for this part.