301-330-115-0: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 3.650 INCHES NOMINAL IN, end_item_identification: F108-CF-100 AND 200 ACFT ENG, engine_section_location: LOW PRESSURE TURBINE, reference_data_and_literature: T.O. 2J-F108-14 FIG 9A IND 527 A, criticality_code_justification: AGAV.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-466-7141, 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 | 3.650 INCHES NOMINAL IN |
| end_item_identification | F108-CF-100 AND 200 ACFT ENG |
| engine_section_location | LOW PRESSURE TURBINE |
| reference_data_and_literature | T.O. 2J-F108-14 FIG 9A IND 527 A |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | BLADE-LPT ROTOR STG 1 |
| NSN | 2840-01-466-7141 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14 FIG 9A IND 527 A |
| OVERALL LENGTH | 3.650 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE-LPT ROTOR STG 1 |
| END ITEM IDENTIFICATION | F108-CF-100 AND 200 ACFT ENG |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.