804351CL23: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: COBALT ALLOY VANE, overall_width: 2.045 INCHES NOMINAL IN, overall_height: 4.153 INCHES NOMINAL IN, overall_length: 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN, special_features: FLOW AREA 1.473 - 1.483.PITCH IS 34DEG 47MIN 28SEC, blade_attachment_method: SLOT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-394-5885, 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.
| material | COBALT ALLOY VANE |
| stage_number | 1 |
| overall_width | 2.045 INCHES NOMINAL IN |
| overall_height | 4.153 INCHES NOMINAL IN |
| overall_length | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN |
| special_features | FLOW AREA 1.473 - 1.483.PITCH IS 34DEG 47MIN 28SEC |
| blade_attachment_method | SLOT |
| end_item_identification | TF-33 |
| engine_section_location | HIGH PRESSURE TURBINE |
| reference_data_and_literature | T.O. 2J-TF33-4 FIG31, IND50 |
| criticality_code_justification | ABMK |
| part_name_assigned_by_controlling_agency | VANE,HPT, 1 STG |
| NSN | 2840-01-394-5885 |
| OVERALL HEIGHT | 4.153 INCHES NOMINAL IN |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | ABMK |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31, IND50 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN |
| OVERALL WIDTH | 2.045 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | FLOW AREA 1.473 - 1.483.PITCH IS 34DEG 47MIN 28SEC |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT, 1 STG |