9547M18G10: ROTOR,TURBINE,AIRCRAFT GAS TURBI.
ROTOR,TURBINE,AIRCRAFT GAS TURBI. Key specifications include design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F110-14, FIG 75; REWKD & REIDENTIFED FROM 9547M18G08, end_item_identification: F110-129 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: HIGH PRESSURE COMPRESSOR, criticality_code_justification: APGF AND CZBJ AND FEAT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-430-0435, 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.
| design_type | AXIAL COMPRESSOR |
| special_features | T.O. 2J-F110-14, FIG 75; REWKD & REIDENTIFED FROM 9547M18G08 |
| end_item_identification | F110-129 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | HIGH PRESSURE COMPRESSOR |
| criticality_code_justification | APGF AND CZBJ AND FEAT |
| NSN | 2840-01-430-0435 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND FEAT |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F110-14, FIG 75; REWKD & REIDENTIFED FROM 9547M18G08 |
| END ITEM IDENTIFICATION | F110-129 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.