6047T81G05: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 22.344 INCHES MINIMUM AND 22.346 INCHES MAXIMUM IN, material: STEEL OVERALL, overall_length: 3.025 INCHES MINIMUM AND 3.030 INCHES MAXIMUM IN, special_features: WAS CASE,TURBINE ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG TF34, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-195-1146, 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 | 22.344 INCHES MINIMUM AND 22.346 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| overall_length | 3.025 INCHES MINIMUM AND 3.030 INCHES MAXIMUM IN |
| special_features | WAS CASE,TURBINE ROTOR,TURBINE ENGINE |
| end_item_identification | ACFT ENG TF34 |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | B50TF15CL-A MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-195-1146 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | B50TF15CL-A MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 22.344 INCHES MINIMUM AND 22.346 INCHES MAXIMUM IN |
| OVERALL LENGTH | 3.025 INCHES MINIMUM AND 3.030 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | WAS CASE,TURBINE ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG TF34 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.