6871447: CASE AND NOZZLE ASSEMBLY,TURBINE.
CASE AND NOZZLE ASSEMBLY,TURBINE. Key specifications include material: CHROMIUM ALLOY OUTER CASE, design_type: AXIAL COMPRESSOR, overall_length: 21.735 INCHES MINIMUM AND 21.745 INCHES MAXIMUM IN, special_features: ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE, end_item_identification: T-56 AIRCRAFT ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-429-5196, 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 | CHROMIUM ALLOY OUTER CASE |
| design_type | AXIAL COMPRESSOR |
| overall_length | 21.735 INCHES MINIMUM AND 21.745 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
| end_item_identification | T-56 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-00-429-5196 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 21.735 INCHES MINIMUM AND 21.745 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
| END ITEM IDENTIFICATION | T-56 AIRCRAFT ENGINE |
| MATERIAL | CHROMIUM ALLOY OUTER CASE |
No substitute or cross-reference records for this part.