4059951: NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.
NOZZLE ASSEMBLY,TURBINE,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, end_item_identification: ACFT.ENG. F100/200, engine_section_location: TURBINE, criticality_code_justification: FEAT, part_name_assigned_by_controlling_agency: ORIGINAL NAME NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-234-0843, 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 | 1 |
| special_features | T.O. 2J-F100-14, FIG 155, IND 30; 1800 CYCLE; 1.730-1.749 SQ. IN. AREA; TURBINE STATOR SUPPORT; REID/REPLACED P/NS 4045951CLL, 4056771CLL AND 4059191CLL |
| end_item_identification | ACFT.ENG. F100/200 |
| engine_section_location | TURBINE |
| criticality_code_justification | FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-234-0843 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| ENGINE SECTION LOCATION | TURBINE |
| END ITEM IDENTIFICATION | ACFT.ENG. F100/200 |
No substitute or cross-reference records for this part.