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The Federal Aviation Administration (FAA) is proposing a new airworthiness directive for specific General Electric (GE) aircraft engines due to a manufacturing issue that risks engine failure. This directive aims to replace certain turbine disks, which were made from metal containing possibly harmful iron inclusions. If the affected parts are not replaced, there could be catastrophic engine damage. Comments on this proposed rule are open until March 17, 2025, allowing stakeholders to provide their input.

The Federal Aviation Administration (FAA) is proposing a change to its earlier rule suggestion regarding General Electric (GE) engines, specifically adding more models to the list of those affected. This proposal aims to prevent unsafe conditions that could happen due to part failures in certain engines, which might lead to engine separation and airplane loss. The FAA is looking for public feedback on this updated proposal by March 10, 2025, and it describes methods for inspecting and repairing the engines to ensure safety.

The Federal Aviation Administration (FAA) has issued a new airworthiness directive (AD) for General Electric Company Model CT7-2E1 engines due to a revised analysis showing that a component, specifically the stage 2 turbine aft cooling plate, has a shorter life than previously thought. This directive requires updating maintenance documents by reducing the life limit for this part from 6,100 cycles to 3,100 cycles to prevent potential failures that could result in severe engine and airplane damage. The rule will take effect on April 17, 2025, and affects eight engines currently used in the U.S.

The Federal Aviation Administration (FAA) has proposed a new airworthiness directive (AD) for certain General Electric engines. This proposal aims to replace specific high-pressure turbine (HPT) disks due to potential iron inclusions, which could lead to fractures and uncontained engine failure. The proposed directive is intended to ensure the safety of these engines by mandating the replacement of affected parts. The FAA invites public comments on this proposal until March 17, 2025.

The Federal Aviation Administration (FAA) has issued a new airworthiness directive (AD) for certain models of General Electric (GE) engines. This directive was prompted by a manufacturer evaluation suggesting that a lower life limit may be needed for specific compressor rotor spools, stages 6-10, to ensure safety. The AD mandates a one-time inspection of these spools to check for compliance with updated repair limits and requires their replacement if they do not meet the necessary standards. The rule is intended to prevent potential engine failures and ensure flight safety.

The Federal Aviation Administration (FAA) has proposed a new safety rule concerning specific models of GE turbofan engines due to reports of cracks in the lower fuel manifold that could lead to fuel leaks and engine fires. The rule requires inspections of this part and, if cracks are found, its replacement with a new one. This action is termed "interim," as a long-term solution is being developed. Stakeholders are invited to submit comments on this proposal by April 12, 2021.

The Federal Aviation Administration (FAA) is proposing a new airworthiness directive for certain General Electric turbofan engines due to safety concerns. Following an inspection, it was found that cracks in the high-pressure turbine rotor components could lead to engine and aircraft damage. The directive would require regular inspections and potentially remove certain parts if cracks are detected. The FAA has invited public comments on this proposed rule until April 8, 2021.

The Federal Aviation Administration (FAA) is enforcing a new airworthiness directive for certain models of General Electric turbofan engines due to a reported crack in the outer fuel manifold leading to fuel leakage. This rule requires initial and routine inspections of specific clamps and may involve further inspections or replacements if defects are found. The purpose is to prevent potential engine fire and aircraft damage. The directive details necessary actions, compliance timelines, and communication procedures for alternative methods or further information.

The Federal Aviation Administration (FAA) issued an airworthiness directive (AD) affecting specific General Electric turbofan engines. This directive was prompted by incidents leading to significant fuel loss and engine shutdowns during flights. To address these issues, the AD mandates initial and repetitive shim checks of specific components and performs tests if necessary, to ensure safety. This measure aims to prevent engine failures and potential hazards to aircraft and passengers.

The North American Electric Reliability Corporation (NERC) submitted its annual report on December 30, 2020, detailing the Find, Fix, Track and Report and Compliance Exception programs as required by the Federal Energy Regulatory Commission (FERC). Interested individuals can intervene or protest this filing according to FERC's rules, though these protests won't grant the status of a party to the protestors. Electronic submissions are preferred, and detailed instructions are provided for accessing the document online. Comments are due by 5:00 p.m. Eastern Time on January 20, 2021.