4068717-700: ROTOR,COMPRESSOR,AIRCRAFT GAS TU.
ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F100-4, FIG 86, IND 1; GOES ON THE COMPRESSOR REAR DRIVE, end_item_identification: F100PW229 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR, criticality_code_justification: FEAT AND CZCJ AND CZBJ AND APGF, part_name_assigned_by_controlling_agency: COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-308-3712, 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 |
| special_features | T.O. 2J-F100-4, FIG 86, IND 1; GOES ON THE COMPRESSOR REAR DRIVE |
| end_item_identification | F100PW229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | FEAT AND CZCJ AND CZBJ AND APGF |
| part_name_assigned_by_controlling_agency | COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |
| NSN | 2840-01-308-3712 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT AND CZCJ AND CZBJ AND APGF |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-4, FIG 86, IND 1; GOES ON THE COMPRESSOR REAR DRIVE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.