9527M50G01: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 5.400 INCHES NOMINAL IN, end_item_identification: F108 ACFT ENG, engine_section_location: HIGH PRESSURE TURBINE, reference_data_and_literature: T.O. 2J-F108-14, FIG 72-51-00, IND 136A A, criticality_code_justification: AGAV.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-466-9348, 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 | 5.400 INCHES NOMINAL IN |
| end_item_identification | F108 ACFT ENG |
| engine_section_location | HIGH PRESSURE TURBINE |
| reference_data_and_literature | T.O. 2J-F108-14, FIG 72-51-00, IND 136A A |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | NOZZLE SEGMENT-HPT STATOR |
| NSN | 2840-01-466-9348 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14, FIG 72-51-00, IND 136A A |
| OVERALL LENGTH | 5.400 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE SEGMENT-HPT STATOR |
| END ITEM IDENTIFICATION | F108 ACFT ENG |
| MATERIAL | NICKEL ALLOY OVERALL |