1359M16G06-110B: ROTOR,COMPRESSOR,AIRCRAFT GAS TU.
ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include diameter: 17.000 INCHES NOMINAL IN, material: NICKEL ALLOY OVERALL, overall_length: 14.500 INCHES NOMINAL IN, end_item_identification: F110-100B 2J-F100-4, engine_section_location: HIGH PRESSURE COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-475-3393, 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 | 17.000 INCHES NOMINAL IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 14.500 INCHES NOMINAL IN |
| special_features | SUPPORTS STAGE 4-9 BLADES,PROVIDEDS SEAL TEETH TO PREVENT AIR RECIRCULATION UNDER STAGES 4-9 VANE SHROUD AND TRANSMITS TORQUE BETWEEN THE HPT SHAFTAND HPC FRONT SHAFT |
| end_item_identification | F110-100B 2J-F100-4 |
| engine_section_location | HIGH PRESSURE COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-475-3393 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 17.000 INCHES NOMINAL IN |
| OVERALL LENGTH | 14.500 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| SPECIAL FEATURES | SUPPORTS STAGE 4-9 BLADES,PROVIDEDS SEAL TEETH TO PREVENT AIR RECIRCULATION UNDER STAGES 4-9 VANE SHROUD AND TRANSMITS TORQUE BETWEEN THE HPT SHAFTAND HPC FRONT SHAFT |
| END ITEM IDENTIFICATION | F110-100B 2J-F100-4 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.