1559M93P04: DISK,FAN,AIRCRAFT GAS TURBINE EN.
DISK,FAN,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 23.255 INCHES MINIMUM AND 23.263 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM IN, special_features: MATL IS TI17, end_item_identification: F110-GE-100,F110-GE-100B,F110-GE-129,F118-GE-100. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-484-0453, 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 | 23.255 INCHES MINIMUM AND 23.263 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| overall_length | 3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM IN |
| special_features | MATL IS TI17 |
| end_item_identification | F110-GE-100,F110-GE-100B,F110-GE-129,F118-GE-100 |
| engine_section_location | FAN |
| NSN | 2840-01-484-0453 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| DIAMETER | 23.255 INCHES MINIMUM AND 23.263 INCHES MAXIMUM IN |
| OVERALL LENGTH | 3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | FAN |
| SPECIAL FEATURES | MATL IS TI17 |
| END ITEM IDENTIFICATION | F110-GE-100,F110-GE-100B,F110-GE-129,F118-GE-100 |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.