1559M63: DISK AND HUB,COMPRESSOR,AIRCRAFT.
DISK AND HUB,COMPRESSOR,AIRCRAFT. Key specifications include diameter: 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM IN, end_item_identification: F118-GE-100 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-322-4759, 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 | 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM IN |
| end_item_identification | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | ABHP AND ABMZ AND FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME HPC COMPRESSOR SPOOL |
| NSN | 2840-01-322-4759 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| OVERALL LENGTH | 6.143 INCHES MINIMUM AND 6.163 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | INCLUDES 1-2 STAGES |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY OUTER CASE |