9525M68G05: ROTOR,FAN,AIRCRAFT GAS TURBINE E.
ROTOR,FAN,AIRCRAFT GAS TURBINE E. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 24.256 INCHES MINIMUM IN, end_item_identification: 2J-F118-4 F-1 I- 3, engine_section_location: LOW PRESSURE COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-497-7477, 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.
| design_type | AXIAL COMPRESSOR |
| overall_length | 24.256 INCHES MINIMUM IN |
| end_item_identification | 2J-F118-4 F-1 I- 3 |
| engine_section_location | LOW PRESSURE COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-497-7477 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 24.256 INCHES MINIMUM IN |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| END ITEM IDENTIFICATION | 2J-F118-4 F-1 I- 3 |
No substitute or cross-reference records for this part.