9654M44P21: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include design_type: COMPRESSOR, stage_number: 11, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, blade_attachment_method: LOCK, end_item_identification: AIRCRAFT ENGINE TF39-GE1A, engine_section_location: HIGH PRESSURE COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-045-4606, 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 | COMPRESSOR |
| stage_number | 11 |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| blade_attachment_method | LOCK |
| end_item_identification | AIRCRAFT ENGINE TF39-GE1A |
| engine_section_location | HIGH PRESSURE COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-045-4606 |
| STAGE NUMBER | 11 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | LOCK |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | AIRCRAFT ENGINE TF39-GE1A |
No substitute or cross-reference records for this part.