4080392: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include design_type: AXIAL COMPRESSOR, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: TURBINE, criticality_code_justification: FEAT AND CZBJ, part_name_assigned_by_controlling_agency: ORIGINAL NAME BLADE SET,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-369-6022, 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 |
| special_features | T.O. 2J-F100-54, FIG 99, IND 14/15; 72 UNITS PER ASSY; USED ON THE REARCOMPRESSOR DRIVE TURBINE ROTOR ASSY; 2OF THESE BLADES MAKE UP P/N 4076972 |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | FEAT AND CZBJ |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME BLADE SET,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-369-6022 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 14/15; 72 UNITS PER ASSY; USED ON THE REARCOMPRESSOR DRIVE TURBINE ROTOR ASSY; 2OF THESE BLADES MAKE UP P/N 4076972 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BLADE SET,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.