1441M65G04: ROTOR,COMPRESSOR,AIRCRAFT GAS TU.
ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY OUTER CASE, design_type: AXIAL COMPRESSOR, overall_length: 14.506 INCHES MINIMUM AND 14.516 INCHES MAXIMUM IN, special_features: INCLUDES 4-9 STAGES, end_item_identification: F110GE129 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-322-4760, 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.
| material | TITANIUM ALLOY OUTER CASE |
| design_type | AXIAL COMPRESSOR |
| overall_length | 14.506 INCHES MINIMUM AND 14.516 INCHES MAXIMUM IN |
| special_features | INCLUDES 4-9 STAGES |
| end_item_identification | F110GE129 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| NSN | 2840-01-322-4760 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| OVERALL LENGTH | 14.506 INCHES MINIMUM AND 14.516 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | INCLUDES 4-9 STAGES |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY OUTER CASE |
No substitute or cross-reference records for this part.