6844618: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 21.221 INCHES MINIMUM AND 21.225 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, overall_length: 6.386 INCHES MINIMUM AND 6.396 INCHES MAXIMUM IN, special_features: 19.878-19.882 IN. ID.
IN, end_item_identification: T56 ENG, engine_section_location: TURBINE. This part is cataloged in the U.S. Government catalog under NSN 2840-00-010-4049, 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 | 21.221 INCHES MINIMUM AND 21.225 INCHES MAXIMUM IN |
| design_type | AXIAL COMPRESSOR |
| overall_length | 6.386 INCHES MINIMUM AND 6.396 INCHES MAXIMUM IN |
| special_features | 19.878-19.882 IN. ID. IN |
| end_item_identification | T56 ENG |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-00-010-4049 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 21.221 INCHES MINIMUM AND 21.225 INCHES MAXIMUM IN |
| OVERALL LENGTH | 6.386 INCHES MINIMUM AND 6.396 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | 19.878-19.882 IN. ID. IN |
| END ITEM IDENTIFICATION | T56 ENG |
No substitute or cross-reference records for this part.