804351CL16: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: COBALT ALLOY VANE, overall_length: 4.980 INCHES MINIMUM AND 5.030 INCHES MAXIMUM IN, special_features: FLOW AREA IS 1.409 MIN. TO 1.418 MAX.
DIAMETER, blade_attachment_method: SLOT, end_item_identification: ACFT ENG TF33, engine_section_location: HIGH PRESSURE TURBINE. This part is cataloged in the U.S. Government catalog under NSN 2840-01-394-5225, 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_length | 4.980 INCHES MINIMUM AND 5.030 INCHES MAXIMUM IN |
| special_features | FLOW AREA IS 1.409 MIN. TO 1.418 MAX. DIAMETER |
| blade_attachment_method | SLOT |
| end_item_identification | ACFT ENG TF33 |
| engine_section_location | HIGH PRESSURE TURBINE |
| reference_data_and_literature | T.O. 2J-TF33-4 FIG 31 IND 50 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | VANE-TURB STTR,1 STG |
| NSN | 2840-01-394-5225 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 4.980 INCHES MINIMUM AND 5.030 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | FLOW AREA IS 1.409 MIN. TO 1.418 MAX. DIAMETER |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE-TURB STTR,1 STG |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| MATERIAL | COBALT ALLOY VANE |