K019G02: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 1.472 INCHES NOMINAL IN, end_item_identification: TF-39 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR, criticality_code_justification: FEAT, part_name_assigned_by_controlling_agency: ORIGINAL NAME BLADE,COMPRESSOR ROTOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-447-2509, 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 | 1 |
| overall_length | 1.472 INCHES NOMINAL IN |
| special_features | MODIFIED BLADE HAS TUNGSTEN CARBIDE WEAR COATING ON THE MIDSPAN SHROUDS AND REPLACES P/NS K159P01, P02, P04, P07 WITH A BRAZED ON CARBALOY WEAR PAD FOR INCREASED WEAR LIFE |
| end_item_identification | TF-39 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME BLADE,COMPRESSOR ROTOR |
| NSN | 2840-01-447-2509 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| OVERALL LENGTH | 1.472 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | MODIFIED BLADE HAS TUNGSTEN CARBIDE WEAR COATING ON THE MIDSPAN SHROUDS AND REPLACES P/NS K159P01, P02, P04, P07 WITH A BRAZED ON CARBALOY WEAR PAD FOR INCREASED WEAR LIFE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BLADE,COMPRESSOR ROTOR |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |