23064880: VANE ASSEMBLY,COMPRESSOR,AIRCRAF.
VANE ASSEMBLY,COMPRESSOR,AIRCRAF. Key specifications include design_type: AXIAL COMPRESSOR, stage_number: 10, surface_treatment: ALUMINUM OVERALL, end_item_identification: T-56 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR, criticality_code_justification: SFTT AND CZBJ AND FEAT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-436-4065, 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 | 10 |
| special_features | T.O. 2J-T56-24, FIG 27, IND 13; COATING IS IVADIZED BASED ON ENVIRONMENTAL CONCERNS AGAINST THE PREVIOUS CADMIUM PLATING ON THE OLD CONFIGURATION P/N 6859610 |
| surface_treatment | ALUMINUM OVERALL |
| end_item_identification | T-56 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | SFTT AND CZBJ AND FEAT |
| NSN | 2840-01-436-4065 |
| STAGE NUMBER | 10 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | SFTT AND CZBJ AND FEAT |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-T56-24, FIG 27, IND 13; COATING IS IVADIZED BASED ON ENVIRONMENTAL CONCERNS AGAINST THE PREVIOUS CADMIUM PLATING ON THE OLD CONFIGURATION P/N 6859610 |
| SURFACE TREATMENT | ALUMINUM OVERALL |
| END ITEM IDENTIFICATION | T-56 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.