6866634: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 10.046 INCHES NOMINAL IN, material: ALUMINUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 1.280 INCHES NOMINAL IN, end_item_identification: TF-41 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-236-5002, 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 | 10.046 INCHES NOMINAL IN |
| material | ALUMINUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 1.280 INCHES NOMINAL IN |
| end_item_identification | TF-41 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | APGF AND CZBJ AND ABHP AND ABMZ |
| material_document_and_classification | AMS4217 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME SEAL,STATIC REAR |
| NSN | 2840-00-236-5002 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND ABHP AND ABMZ |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4217 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 10.046 INCHES NOMINAL IN |
| OVERALL LENGTH | 1.280 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL,STATIC REAR |
| END ITEM IDENTIFICATION | TF-41 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | ALUMINUM ALLOY OVERALL |