305-350-057-0: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 4.000 INCHES NOMINAL IN, special_features: MATERIAL RENE77, end_item_identification: F108 AIRCRAFT ENGINE, engine_section_location: LOW PRESSURE TURBINE, reference_data_and_literature: T.O. 2J-F108-14 FIG 72-53-00-10 IND 110K.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-344-9156, 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 |
| stage_number | 1 |
| overall_length | 4.000 INCHES NOMINAL IN |
| special_features | MATERIAL RENE77 |
| end_item_identification | F108 AIRCRAFT ENGINE |
| engine_section_location | LOW PRESSURE TURBINE |
| reference_data_and_literature | T.O. 2J-F108-14 FIG 72-53-00-10 IND 110K |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | NOZZLE SEGMENT-LPT STG 1 |
| NSN | 2840-01-344-9156 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14 FIG 72-53-00-10 IND 110K |
| OVERALL LENGTH | 4.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | MATERIAL RENE77 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE SEGMENT-LPT STG 1 |
| END ITEM IDENTIFICATION | F108 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |