4054752: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 2.258 INCHES MINIMUM AND 2.282 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-14, FIG 153, IND 22; 1800 CYCLE; 2.393-2.412 SQ.
IN. AREA; REPLACED P/NS 4051852CLD, end_item_identification: ACFT ENG F100, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-120-1949, 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 | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 2 |
| overall_length | 2.258 INCHES MINIMUM AND 2.282 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-14, FIG 153, IND 22; 1800 CYCLE; 2.393-2.412 SQ. IN. AREA; REPLACED P/NS 4051852CLD |
| end_item_identification | ACFT ENG F100 |
| engine_section_location | TURBINE |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME VANE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-120-1949 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| OVERALL LENGTH | 2.258 INCHES MINIMUM AND 2.282 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 153, IND 22; 2.412-2.432 SQ. IN. AREA; 1800 CYCLE; TURBINE DISK AND HUB; SUPERSEDES P/N 4051852CLE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME VANE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.