4051852CLC: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY VANE, design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F100-14, FIG 153, IND 22; 1800 CYCLE; 2.373-2.393 SQ.
IN. AREA; REPLACED BY P/N 4054752CLC, end_item_identification: ACFT ENG F100-P100, engine_section_location: TURBINE, criticality_code_justification: FEAT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-070-0334, 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 | NICKEL ALLOY VANE |
| design_type | AXIAL COMPRESSOR |
| stage_number | 2 |
| special_features | T.O. 2J-F100-14, FIG 153, IND 22; 1800 CYCLE; 2.373-2.393 SQ. IN. AREA; REPLACED BY P/N 4054752CLC |
| end_item_identification | ACFT ENG F100-P100 |
| engine_section_location | TURBINE |
| criticality_code_justification | FEAT |
| material_document_and_classification | PWA1422 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-070-0334 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1422 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 153, IND 22; 1800 CYCLE; 2.373-2.393 SQ. IN. AREA; REPLACED BY P/N 4054752CLC |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100-P100 |
| MATERIAL | NICKEL ALLOY VANE |