305-390-404-0: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 9.000 INCHES NOMINAL IN, special_features: MATERIAL J-F108-14 FIG 72-54-00-09, IND 280C, end_item_identification: ACFT ENG F108, engine_section_location: LOW PRESSURE TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-185-6496, 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 OVERALL |
| overall_length | 9.000 INCHES NOMINAL IN |
| special_features | MATERIAL J-F108-14 FIG 72-54-00-09, IND 280C |
| end_item_identification | ACFT ENG F108 |
| engine_section_location | LOW PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | NOZZLE SEG ASSY-LPT STG 2 |
| NSN | 2840-01-185-6496 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 9.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | MATERIAL J-F108-14 FIG 72-54-00-09, IND 280C |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE SEG ASSY-LPT STG 2 |
| END ITEM IDENTIFICATION | ACFT ENG F108 |
| MATERIAL | NICKEL ALLOY OVERALL |