2411M21G01-2A: DISK,COMPRESSOR,AIRCRAFT GAS TUR.
DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: TITANIUM OVERALL, design_type: AXIAL-CENTRIFUGAL, special_features: LIFE LIMITED PART, end_item_identification: CFM56, engine_section_location: COMPRESSOR, reference_data_and_literature: T.O.2J-F108-14 FIG 72-31-00-1 IND140D. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-519-2631, 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 OVERALL |
| design_type | AXIAL-CENTRIFUGAL |
| stage_number | 1 |
| special_features | LIFE LIMITED PART |
| end_item_identification | CFM56 |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O.2J-F108-14 FIG 72-31-00-1 IND140D |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | SPOOL-STAGE 1AND 2 |
| NSN | 2840-01-519-2631 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL-CENTRIFUGAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O.2J-F108-14 FIG 72-31-00-1 IND140D |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | LIFE LIMITED PART |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SPOOL-STAGE 1AND 2 |
| END ITEM IDENTIFICATION | CFM56 |
| MATERIAL | TITANIUM OVERALL |