1385M70G02: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, special_features: 2 BLADE ASSEMBLY, end_item_identification: ACFT ENG F108, engine_section_location: TURBINE, reference_data_and_literature: 2F-F108-14, criticality_code_justification: CZBJ AND FEAT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-274-9388, 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 |
| special_features | 2 BLADE ASSEMBLY |
| end_item_identification | ACFT ENG F108 |
| engine_section_location | TURBINE |
| reference_data_and_literature | 2F-F108-14 |
| criticality_code_justification | CZBJ AND FEAT |
| part_name_assigned_by_controlling_agency | NOZZLE SEGMENT-HPT STATOR |
| NSN | 2840-01-274-9388 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND FEAT |
| REFERENCE DATA AND LITERATURE | 2F-F108-14 |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | 2 BLADE ASSEMBLY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE SEGMENT-HPT STATOR |
| END ITEM IDENTIFICATION | ACFT ENG F108 |
No substitute or cross-reference records for this part.