9531M23P05: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY OVERALL, overall_length: 3.011 INCHES NOMINAL IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG F110, engine_section_location: COMPRESSOR, reference_data_and_literature: T.O. 2J-110-4.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-200-5347, 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 | TITANIUM ALLOY OVERALL |
| stage_number | 3 |
| overall_length | 3.011 INCHES NOMINAL IN |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | ACFT ENG F110 |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-110-4 |
| part_name_assigned_by_controlling_agency | BLADE,FAN ROTOR-STG 3 |
| NSN | 2840-01-200-5347 |
| STAGE NUMBER | 3 |
| REFERENCE DATA AND LITERATURE | T.O. 2J-110-4 |
| OVERALL LENGTH | 3.011 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,FAN ROTOR-STG 3 |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.