658930: BAFFLE,AIRFLOW,AIRCRAFT GAS TURB.
BAFFLE,AIRFLOW,AIRCRAFT GAS TURB. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 2.877 INCHES MINIMUM AND 2.897 INCHES MAXIMUM IN, special_features: T.O. 2J-TF30-44, FIG 28, IND 36, end_item_identification: TF-30 AIRCRAFT ENGINE, engine_section_location: TURBINE, criticality_code_justification: AGAV.
This part is cataloged in the U.S. Government catalog under NSN 2840-00-444-4950, 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 |
| overall_length | 2.877 INCHES MINIMUM AND 2.897 INCHES MAXIMUM IN |
| special_features | T.O. 2J-TF30-44, FIG 28, IND 36 |
| end_item_identification | TF-30 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME BAFFLE,STATOR VANE |
| NSN | 2840-00-444-4950 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 2.877 INCHES MINIMUM AND 2.897 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-TF30-44, FIG 28, IND 36 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BAFFLE,STATOR VANE |
| END ITEM IDENTIFICATION | TF-30 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.