638E259P6: SHAFT,TURBINE,AIRCRAFT GAS TURBI.
SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include diameter: 8.461 INCHES MINIMUM AND 8.469 INCHES MAXIMUM IN, material: STEEL OVERALL, overall_length: 4.843 INCHES MINIMUM AND 4.845 INCHES MAXIMUM IN, end_item_identification: ACFT ENG, engine_section_location: COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-110-8019, 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 | 8.461 INCHES MINIMUM AND 8.469 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| overall_length | 4.843 INCHES MINIMUM AND 4.845 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | SHAFT STUB, COMPRESSOR ROTOR, FRONT |
| NSN | 2840-00-110-8019 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 8.461 INCHES MINIMUM AND 8.469 INCHES MAXIMUM IN |
| OVERALL LENGTH | 4.843 INCHES MINIMUM AND 4.845 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHAFT STUB, COMPRESSOR ROTOR, FRONT |
| END ITEM IDENTIFICATION | ACFT ENG |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.