660917: BAFFLE,AIRFLOW,AIRCRAFT GAS TURB.
BAFFLE,AIRFLOW,AIRCRAFT GAS TURB. Key specifications include diameter: 8.895 INCHES MINIMUM AND 8.905 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 2.647 INCHES MINIMUM AND 2.649 INCHES MAXIMUM IN, end_item_identification: TF30 AIRCRAFT GAS TURBINE ENG, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-412-0308, 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 | 8.895 INCHES MINIMUM AND 8.905 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| overall_length | 2.647 INCHES MINIMUM AND 2.649 INCHES MAXIMUM IN |
| end_item_identification | TF30 AIRCRAFT GAS TURBINE ENG |
| engine_section_location | TURBINE |
| criticality_code_justification | ABHP AND ABMZ AND CZCJ |
| material_document_and_classification | PWA1007 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME BAFFLE,TURBINE,TURBINE ENGINE |
| NSN | 2840-00-412-0308 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND CZCJ |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1007 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 8.895 INCHES MINIMUM AND 8.905 INCHES MAXIMUM IN |
| OVERALL LENGTH | 2.647 INCHES MINIMUM AND 2.649 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BAFFLE,TURBINE,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF30 AIRCRAFT GAS TURBINE ENG |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.