9547M19G08: ROTOR,TURBINE,AIRCRAFT GAS TURBI.
ROTOR,TURBINE,AIRCRAFT GAS TURBI. Key specifications include design_type: AXIAL COMPRESSOR, end_item_identification: F110-GE-129 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: LOW PRESSURE TURBINE, criticality_code_justification: FEAT AND CZBJ, part_name_assigned_by_controlling_agency: ORIGINAL NAME ROTOR ASSEMBLY,LOW PRESSURE TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-447-2504, 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 |
| end_item_identification | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | LOW PRESSURE TURBINE |
| criticality_code_justification | FEAT AND CZBJ |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME ROTOR ASSEMBLY,LOW PRESSURE TURBINE |
| NSN | 2840-01-447-2504 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | MATERIAL IS A CRYSTAL RENE N6, A PRECIPITATION STRENGTHENED ALLOY; ROTOR HAS A NEW REDESIGNED STG 1 BLADE WITH THE NEW MATERIAL; INCREASED LIFE OF BLADE; BLADES ARE STILL DOVETAIL AND ARE IDENTICAL TO THE OLD CONFIGURATION P/N 1475M47P01; NEW BLADES ARE INTERCHANGEABLE IN COMPLETE SETS ONLY; INTERMIXING OF BLADES, OLD AND NEW, WILL NOTBE ALLOWED; SINCE DOVETAILS ARE IDENTICAL AND WILL FIT IN THE SAME DISK, NO CHANGES TO DISK |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME ROTOR ASSEMBLY,LOW PRESSURE TURBINE |
| END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |