2840PL0728530: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include design_type: AXIAL COMPRESSOR, end_item_identification: ACFT ENG F100299, engine_section_location: TURBINE, criticality_code_justification: AGAV, part_name_assigned_by_controlling_agency: BLADE SET TURBINE ROTOR, 1 STAGE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-462-3954, 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 | 1 |
| special_features | BLADE SET 4086361 SUPERSEDES 4087101 (2840014456144PT) BY ATTRITION, NOTECHINICAL ORDER DATA AVAILABLE, 2 BLADES REQUIRED AND MUST BE SAME MOMENT WT WITHIN 0.050 OZ. IN. OZ |
| end_item_identification | ACFT ENG F100299 |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | BLADE SET TURBINE ROTOR, 1 STAGE |
| NSN | 2840-01-462-3954 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | BLADE SET 4086361 SUPERSEDES 4087101 (2840014456144PT) BY ATTRITION, NOTECHINICAL ORDER DATA AVAILABLE, 2 BLADES REQUIRED AND MUST BE SAME MOMENT WT WITHIN 0.050 OZ. IN. OZ |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE SET TURBINE ROTOR, 1 STAGE |
| END ITEM IDENTIFICATION | ACFT ENG F100299 |
No substitute or cross-reference records for this part.