9835252-10: DISK AND HUB,TURBINE,AIRCRAFT GA.
DISK AND HUB,TURBINE,AIRCRAFT GA. Key specifications include design_type: AXIAL COMPRESSOR, special_features: T.O.2J-TF33-34 FIG. 5B INDEX 1B, HUB AND BLADE ASSEMBLY FRONT COMPRESSOR, end_item_identification: ACFT ENG TF33-34, engine_section_location: COMPRESSOR, criticality_code_justification: AGAV, part_name_assigned_by_controlling_agency: DISK AND BLADE ASSEMBLY, 1ST STAGE COMPRESSOR.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-460-4376, 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 |
| special_features | T.O.2J-TF33-34 FIG. 5B INDEX 1B, HUB AND BLADE ASSEMBLY FRONT COMPRESSOR |
| end_item_identification | ACFT ENG TF33-34 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | DISK AND BLADE ASSEMBLY, 1ST STAGE COMPRESSOR |
| NSN | 2840-01-460-4376 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O.2J-TF33-34 FIG. 5B INDEX 1B, HUB AND BLADE ASSEMBLY FRONT COMPRESSOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DISK AND BLADE ASSEMBLY, 1ST STAGE COMPRESSOR |
| END ITEM IDENTIFICATION | ACFT ENG TF33-34 |
No substitute or cross-reference records for this part.