9835252-30: 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 1A,HUB AND BLADE ASSEMBLY FRONT COMPRESSOR, NOTE: USED ON TF33-102C, 1ST STAGE A, end_item_identification: ACFT ENG TF33-102C, engine_section_location: COMPRESSOR, criticality_code_justification: AGAV, part_name_assigned_by_controlling_agency: DISK AND BLADE ASSEMBLY 1ST STAGECOMPRESSOR.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-460-4380, 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 1A,HUB AND BLADE ASSEMBLY FRONT COMPRESSOR, NOTE: USED ON TF33-102C, 1ST STAGE A |
| end_item_identification | ACFT ENG TF33-102C |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | DISK AND BLADE ASSEMBLY 1ST STAGECOMPRESSOR |
| NSN | 2840-01-460-4380 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O.2J-TF33-34 FIG. 5B, INDEX 1A,HUB AND BLADE ASSEMBLY FRONT COMPRESSOR, NOTE: USED ON TF33-102C, 1ST STAGE A |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DISK AND BLADE ASSEMBLY 1ST STAGECOMPRESSOR |
| END ITEM IDENTIFICATION | ACFT ENG TF33-102C |
No substitute or cross-reference records for this part.