9521M14G18: ROTOR,COMPRESSOR,AIRCRAFT GAS TU.
ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, design_type: COMPRESSOR, special_features: FSCAP;BLADE IS CROPPED BY 0.300 OFF TOPSIDE;T.O. 2J-F110-4,FIG 1,IND 10;TCTO 2J-F110-607, end_item_identification: F110 AIRCRAFT ENGINE, engine_section_location: HIGH PRESSURE COMPRESSOR, criticality_code_justification: FEAT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-330-9053, 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 | STEEL BLADE |
| design_type | COMPRESSOR |
| stage_number | 3 |
| special_features | FSCAP;BLADE IS CROPPED BY 0.300 OFF TOPSIDE;T.O. 2J-F110-4,FIG 1,IND 10;TCTO 2J-F110-607 |
| end_item_identification | F110 AIRCRAFT ENGINE |
| engine_section_location | HIGH PRESSURE COMPRESSOR |
| criticality_code_justification | FEAT |
| NSN | 2840-01-330-9053 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| SPECIAL FEATURES | FSCAP;BLADE IS CROPPED BY 0.300 OFF TOPSIDE;T.O. 2J-F110-4,FIG 1,IND 10;TCTO 2J-F110-607 |
| END ITEM IDENTIFICATION | F110 AIRCRAFT ENGINE |
| MATERIAL | STEEL BLADE |