6866701: BAFFLE,AIRFLOW,AIRCRAFT GAS TURB.
BAFFLE,AIRFLOW,AIRCRAFT GAS TURB. Key specifications include diameter: 18.000 INCHES MINIMUM AND 18.025 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, stage_number: 11, overall_length: 0.320 INCHES MINIMUM AND 0.345 INCHES MAXIMUM IN, end_item_identification: TF41 ACFT GAS TURBINE ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-403-0693, 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.
| diameter | 18.000 INCHES MINIMUM AND 18.025 INCHES MAXIMUM IN |
| design_type | AXIAL COMPRESSOR |
| stage_number | 11 |
| overall_length | 0.320 INCHES MINIMUM AND 0.345 INCHES MAXIMUM IN |
| end_item_identification | TF41 ACFT GAS TURBINE ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | CZBJ AND ABHP AND ABMZ |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME RING,ANNULUS,DIFFUSER |
| NSN | 2840-00-403-0693 |
| STAGE NUMBER | 11 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND ABMZ |
| DIAMETER | 18.000 INCHES MINIMUM AND 18.025 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.320 INCHES MINIMUM AND 0.345 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME RING,ANNULUS,DIFFUSER |
| END ITEM IDENTIFICATION | TF41 ACFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.