1807M15: DAMPER,TURBINE BLADE,AIRCRAFT TU.
DAMPER,TURBINE BLADE,AIRCRAFT TU. Key specifications include design_type: AXIAL COMPRESSOR, special_features: ORIGINAL NAME DAMPER ASSEMBLY,HIGH PRESSURE TURBINE ROTOR-STAGE 2. ALSOPART NUMBER G05 ADDED PER CID 219639, end_item_identification: ACFT ENG TF39, engine_section_location: HIGH PRESSURE TURBINE, criticality_code_justification: AGAV.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-444-6530, 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 |
| stage_number | 2 |
| special_features | ORIGINAL NAME DAMPER ASSEMBLY,HIGH PRESSURE TURBINE ROTOR-STAGE 2. ALSOPART NUMBER G05 ADDED PER CID 219639 |
| end_item_identification | ACFT ENG TF39 |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-444-6530 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | ORIGINAL NAME DAMPER ASSEMBLY,HIGH PRESSURE TURBINE ROTOR-STAGE 2. ALSOPART NUMBER G05 ADDED PER CID 219639 |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |
No substitute or cross-reference records for this part.