EASA AD US-2022-08-06
Engine - Compressor Inlet Guide Vane Outer Shroud Bushing and Vane Spindle Bushing - Inspection / Replacement
The document titled "Engine - Compressor Inlet Guide Vane Outer Shroud Bushing and Vane Spindle Bushing - Inspection / Replacement" is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2022-08-06) addressing certain General Electric Company CF34-8C and CF34-8E turbofan engines. It mandates inspections and potential replacements related to corrosion issues in the variable geometry system actuator that can cause engine control problems. The AD aims to prevent engine failures and loss of thrust control on affected aircraft such as Bombardier CRJ1000 and CRJ900 models powered by these engines.
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric CF34-8Bombardier CRJ1000Bombardier CRJ900