4060952CLF: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F100-14, FIG 153, IND 22; 2.432-2.452 SQ.
IN. AREA; 1800 CYCLE; REPLACED BY P/N 4054752CLF, end_item_identification: ACFT ENG F100/200, engine_section_location: TURBINE, criticality_code_justification: FEAT, part_name_assigned_by_controlling_agency: ORIGINAL NAME VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-151-0374, 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 | 2 |
| special_features | T.O. 2J-F100-14, FIG 153, IND 22; 2.432-2.452 SQ. IN. AREA; 1800 CYCLE; REPLACED BY P/N 4054752CLF |
| end_item_identification | ACFT ENG F100/200 |
| engine_section_location | TURBINE |
| criticality_code_justification | FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-151-0374 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 153, IND 22; 2.432-2.452 SQ. IN. AREA; 1800 CYCLE; REPLACED BY P/N 4054752CLF |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100/200 |