1441M60P07: DISK,COMPRESSOR,AIRCRAFT GAS TUR.
DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: TITANIUM ALLOY DISK, design_type: AXIAL COMPRESSOR, overall_length: 11.953 INCHES NOMINAL IN, special_features: SPLINE DATA: NO. OF TEETH 50; PITCH DIA.
5.102; PRESSURE ANGLE 14 DEG. 30 MIN.; O/A DIA. 5.040, end_item_identification: F110GE129 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-322-4758, 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 DISK |
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| overall_length | 11.953 INCHES NOMINAL IN |
| special_features | SPLINE DATA: NO. OF TEETH 50; PITCH DIA. 5.102; PRESSURE ANGLE 14 DEG. 30 MIN.; O/A DIA. 5.040 |
| end_item_identification | F110GE129 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| NSN | 2840-01-322-4758 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| OVERALL LENGTH | 11.953 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | SPLINE DATA: NO. OF TEETH 50; PITCH DIA. 5.102; PRESSURE ANGLE 14 DEG. 30 MIN.; O/A DIA. 5.040 |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY DISK |