Regulations & Safety
FAA Proposes New Airworthiness Directive for GE CF34 Engines After Naples Crash
FAA proposes strict inspections for GE CF34 engines following a fatal Naples crash caused by corrosion in the variable geometry system. Comments open until June 15.

FAA Proposes Strict New Airworthiness Directive for GE CF34 Engines Following Fatal Naples Crash
The Federal Aviation Administration (FAA) has officially issued a Notice of Proposed Rulemaking (NPRM) that would mandate stringent new inspection and maintenance protocols for specific General Electric (GE) CF34 turbofan engines. According to the FAA document, the proposed Airworthiness Directive (AD) is designed to address a critical safety vulnerability involving hidden corrosion within the engine’s high-pressure compressor (HPC) case, a condition that can lead to an uncommanded loss of thrust.
This sweeping regulatory action is a direct response to the fatal crash of a Hop-A-Jet Bombardier Challenger 604 in Naples, Florida, on February 9, 2024. The National Transportation Safety Board (NTSB) recently concluded that the accident was caused by the exact mechanical failure targeted in this new FAA proposal.
At AirPro News, we are closely monitoring how this proposed directive will impact operators. The rule threatens to introduce significant new maintenance burdens for fleets utilizing the affected GE engines, primarily Bombardier Challenger 600-series business jets and CRJ200-family regional jets. We have broken down the regulatory actions, the NTSB findings, and the broader implications for the aviation industry.
The Triggering Event: Hop-A-Jet Flight 823
The catalyst for the FAA’s proposed AD was the tragic loss of Hop-A-Jet Flight 823. On February 9, 2024, the Bombardier Challenger 604 (registration N823KD) experienced a simultaneous dual-engine failure while on approach to Naples Municipal Airport. According to the NTSB investigation records, the flight crew declared an emergency and attempted an off-airport landing on Interstate 75. The aircraft collided with vehicles, resulting in a post-crash fire. Both pilots were killed in the accident, while the flight attendant, two passengers, and a motorist on the ground survived with injuries.
NTSB Findings and Maintenance Shortfalls
The NTSB released its final investigation report on April 23, 2026. The safety board determined that the probable cause of the crash was extensive corrosion in the variable geometry (VG) system components of both GE CF34-3B engines. The NTSB report detailed that this corrosion restricted the movement of the VG hardware, which subsequently led to near-simultaneous, sub-idle rotating compressor stalls and an unrecoverable loss of thrust at a low altitude. Investigators noted that the aircraft was frequently stored in marine climates, exposing it to salty air conditions that accelerate corrosion.
Crucially, the NTSB cited inadequate fault-isolation guidance from the engine manufacturer, GE, as a contributing factor. According to the safety board, this lack of guidance prevented maintenance crews from identifying the corrosion buildup when they were troubleshooting “hung-start” events on the aircraft approximately one month prior to the fatal accident.
FAA’s Proposed Regulatory Action
In response to the NTSB’s findings, the FAA published NPRM Docket No. FAA-2026-3875 on April 30, 2026. The agency is currently accepting public comments on the proposed rule until June 15, 2026. According to the FAA document, the proposed AD applies to GE Model CF34-1A, CF34-3A, CF34-3A1, CF34-3A2, and CF34-3B engines. The FAA estimates that this directive will affect approximately 1,152 engines currently in service.
The FAA has explicitly identified the unsafe condition as corrosion in the HPC case variable vane spindle bores, which restricts the VG system’s range of motion. The agency warns that this restriction can lead to compressor instability at or below idle speeds, potentially resulting in a loss of engine thrust control.
Mandated Inspections and Thresholds
To mitigate this risk, the FAA proposes mandating several strict maintenance actions based on GE Service Bulletin CF34-BJ 72-0347, Revision 02, which was issued on October 30, 2025. According to the NPRM, operators would be required to perform repetitive engine heat soak restart tests every three months. Additionally, maintenance crews must conduct targeted borescope inspections (BSI) of the HPC case to detect corrosion, perform VG system functional checks for pressure evaluation, and conduct force gage tests on the feedback cable.
The proposed rule establishes strict operational thresholds. For example, the FAA stipulates that if the pressure required to fully extend or retract the actuator exceeds 65 psi, the engine must be removed from service entirely. Furthermore, operators will be required to revise the airworthiness limitations section (ALS) of their existing engine maintenance manuals to permanently incorporate these checks.
Stakeholder Pushback and Ongoing Litigation
The proposed AD and the circumstances surrounding the Naples crash have generated significant friction between operators and manufacturers. Hop-A-Jet CEO Barry Ellis has publicly criticized the maintenance protocols that were in place prior to the accident. Ellis noted that GE performed a 3,200-hour borescope inspection on the accident aircraft’s engines in September 2023, less than six months before the crash, and argued that severe corrosion should have been detected during that routine check.
According to public remarks by Hop-A-Jet CEO Barry Ellis, the provided maintenance troubleshooting tree never directed mechanics to pressure-test the VG system.
The fallout from the accident has also moved into the legal arena. In late 2025, Hop-A-Jet Worldwide Jet Charter filed a class-action lawsuit against GE Aerospace, Bombardier Inc., Learjet Inc., and other aviation service providers. According to public legal filings, the lawsuit alleges negligence and concealment, claiming that the manufacturers had been aware since 2019 that the VG system in the CF34 engine family was prone to hidden corrosion.
Broader Industry Impact
AirPro News analysis
If adopted as a final rule, we anticipate that this Airworthiness Directive will fundamentally alter the maintenance economics for operators of legacy Challenger 600-series and CRJ200 aircraft. The requirement to perform quarterly heat soak restart tests, combined with the strict 65 psi pressure threshold for the VG system actuator, introduces a high degree of operational unpredictability.
We assess that depending on the engine type and serial number, owners could be forced to complete initial inspections before further flight or within a one-to-two-year window. Because HPC case overhauls and engine replacements are highly capital-intensive, we expect that these new mandates could lead to the early retirement of older airframes that exhibit severe corrosion, as the cost of compliance may exceed the residual value of the aircraft.
Frequently Asked Questions (FAQ)
Which aircraft are affected by the proposed FAA directive?
According to the FAA NPRM, the directive affects GE Model CF34-1A, CF34-3A, CF34-3A1, CF34-3A2, and CF34-3B engines. These engines primarily power Bombardier Challenger 600-series business jets and CRJ200-family regional jets.
What caused the Hop-A-Jet crash in Naples, Florida?
The NTSB determined the probable cause was extensive corrosion in the variable geometry (VG) system components of both engines, which restricted hardware movement and caused near-simultaneous compressor stalls and a total loss of thrust.
When is the deadline to comment on the FAA’s proposed rule?
The FAA is accepting public comments on Docket No. FAA-2026-3875 until June 15, 2026.
Sources:
Federal Aviation Administration (FAA) Notice of Proposed Rulemaking, Docket No. FAA-2026-3875
National Transportation Safety Board (NTSB) Final Investigation Report (April 23, 2026)
GE Service Bulletin CF34-BJ 72-0347, Revision 02
Photo Credit: GE Aerospace
Regulations & Safety
NTSB Preliminary Report: Ryanair 737-800 Engine Failure
NTSB confirms fan-blade-out on Ryanair 737-800 shattered cabin window, partially ejecting a passenger during climb from Thessaloniki.

This is a developing story. Information may change as official details are released.
This is original reporting and analysis by AirPro News.
On August 13, 2026, the National Transportation Safety Board (NTSB) issued its preliminary report on a July 10 uncontained engine failure aboard a Ryanair Boeing 737-800, confirming that a fan-blade-out event shattered a cabin window and caused a rapid decompression. The incident resulted in a 61-year-old male passenger being partially pulled through the shattered window before being secured by fellow passengers.
The event occurred during climb out from Thessaloniki International Airport (SKG) in Greece. The flight, operated by Ryanair subsidiary Malta Air, was bound for Memmingen, Germany (FMM). The NTSB is currently investigating potential similarities between this event and a fatal 2018 engine failure, while the agency has also publicly addressed premature speculation regarding the cause by Ryanair leadership.
Flight 1879 rapid decompression
According to the NTSB preliminary report, the Boeing 737-800 was climbing when the right-hand CFM56-7B engine experienced a fan-blade-out event. Debris from the engine struck the fuselage and shattered a window at row 11. The resulting rapid decompression pulled a passenger partially outside the aircraft. The passenger sustained neck and shoulder injuries as well as friction burns, but no fatalities occurred.
Reporting by The Air Current indicates the failure happened at an altitude of approximately 15,000 feet. Passengers described a sudden and violent disruption to the flight. A passenger told AP News that the cabin was quiet before a loud noise resembling a bursting tire occurred, adding that they knew immediately the aircraft had lost pressure due to the sudden loss of altitude.
Initial reports following the July 10 incident suggested the failure occurred in the airspace of the Republic of North Macedonia. However, flight path analysis confirmed the event took place in Greek airspace. The Hellenic Air and Rail Safety Investigation Authority officially delegated the investigation to the NTSB on July 16, 2026.
Maintenance history and preliminary findings
The NTSB preliminary report notes that bird remains were found inside the damaged engine. Flight crews had reported four suspected bird strikes to the aircraft’s number two engine in the 12 months preceding the accident. The report states that bird remains were found in two of those previous cases.
Maintenance records indicate that the fan blades on the failed right engine underwent ultrasonic inspections in November 2025 and May 2026. No damage was found during either inspection. The official cause of the July 10 failure remains under investigation by the NTSB, with participation from the Federal Aviation Administration (FAA), Boeing, and CFM International, a joint venture between GE Aerospace and Safran.
Regulatory protocols and historical precedent
The investigation has generated friction between the NTSB and Ryanair regarding public communications. On August 7, 2026, NTSB Chair Jennifer Homendy issued a letter to Ryanair CEO Michael O’Leary after he told investors the investigation was focused on foreign object damage rather than aircraft age or maintenance. Homendy stated that the NTSB had made no such determination and noted that O’Leary’s comments violated International Civil Aviation Organization (ICAO) Annex 13 protocols governing accident investigations.
The aviation industry is closely monitoring the investigation due to the aircraft and engine types involved. The Air Current reported that the event closely mirrors the April 2018 Southwest Airlines flight 1380 uncontained engine failure, which also involved a Boeing 737-700 and a CFM56-7B engine. That incident resulted in one passenger fatality after a shattered window caused partial ejection, leading the FAA to mandate engine inlet redesigns by July 2028.
The NTSB addressed the historical context directly in its preliminary report:
The investigative team is aware of previous … events with similar engine models that resulted in damage to engine inlets or cowlings and fuselage structures. Determination of any relevant similarities or details between this accident and previous events remains under investigation.
AirPro News analysis
We observe that the public rebuke of a major airline CEO by the NTSB is a rare and significant enforcement of ICAO Annex 13 communication protocols. Operators typically defer entirely to the investigating authority to avoid compromising the integrity of an active probe. The NTSB’s swift correction underscores the agency’s zero-tolerance policy for operator speculation, particularly when an event involves high-profile safety concerns like uncontained engine failures.
The CFM56-7B is one of the most widely used commercial aviation engines in the world. Any investigation involving a fan-blade-out event on this powerplant will naturally draw intense regulatory scrutiny, especially given the precedent set by the 2018 Southwest Airlines accident. While the discovery of bird remains introduces foreign object damage as a variable, we expect investigators will rigorously examine the efficacy of the ultrasonic inspections conducted in November 2025 and May 2026 to understand how the blade failure propagated.
Sources: National Transportation Safety Board
Photo Credit: NTSB
Regulations & Safety
FAA Installs New Surface Radar at Newark Airport
The FAA unveiled a new SMR-4 radar at Newark Liberty as part of a $30 million infrastructure upgrade targeting runway safety.

U.S. Transportation Secretary Sean P. Duffy and Federal Aviation Administration (FAA) Administrator Bryan Bedford unveiled a new Surface Movement Radar-Systems Model 4 (SMR-4) at Newark Liberty International Airport (EWR) on August 11, 2026, replacing a 30-year-old legacy system.
The installation is part of a broader $30 million infrastructure upgrade at the New Jersey hub designed to prevent runway incursions and reduce delays. According to the FAA press release, the SMR-4 allows air traffic controllers to track aircraft and ground vehicles across runways and taxiways in all weather and visibility conditions.
Newark’s infrastructure modernization
The $30 million funding allocation for EWR spans a three-year period and targets critical technological vulnerabilities. During the summer of 2025, the Airports experienced severe delays that prompted the FAA to deploy Software patches, expedite fiber deployment, and rebalance flight volumes. To date, 90% of the airport’s legacy copper wiring has been replaced with high-speed fiber.
“Since the start of this administration, we have been working towards building a modern system that will serve America’s skies for generations,” Duffy stated. “From replacing Newark’s ancient copper wire to investing $30 million into new infrastructure and bringing new radar online, we are delivering real safety and efficiency enhancements at one of our nation’s busiest airports.”
The FAA has set a target deadline of summer 2027 for EWR to install new electronic information displays, upgraded voice switches, and a new long-range radar system.
National surface awareness rollout
The EWR installation is one of five SMR-4 systems deployed nationwide to date. The agency has accelerated its broader technological overhaul over the past year, replacing 60% of all copper wires in its national network and converting 363 radio sites. The FAA also transitioned 19 air traffic control towers to electronic flight strips and installed 151 IP voice switches at control towers across the country.
Bedford emphasized the operational volume driving the upgrades. “Newark sees well-over a thousand flights per day, and the new Surface Movement Radar will help controllers keep those flights safe at this major U.S. hub,” Bedford said, describing the deployment as a step toward modernizing the national airspace.
The push for enhanced surface surveillance follows a fatal runway incursion at LaGuardia Airport (LGA) on March 22, 2026. In that event, Air Canada (AC) Express Flight 8646, operated by Jazz Aviation using a Bombardier CRJ900, collided with an airport firefighting vehicle on Runway 4. The National Transportation Safety Board (NTSB) confirmed two pilot fatalities and 39 injuries. The NTSB is leading the ongoing Investigation, and no official cause has been determined.
In response to surface safety concerns, the FAA has installed 96 new Surface Awareness Initiative systems nationwide over the past year to provide controllers with better situational awareness.
AirPro News analysis
The FAA’s rapid deployment of 96 Surface Awareness Initiative systems and the ongoing SMR-4 rollout represent a tangible shift toward proactive technological intervention in ground operations. While the NTSB has not yet concluded its investigation into the March 2026 LaGuardia runway incursion, the agency’s aggressive timeline for replacing legacy copper wiring and installing surface tracking tools indicates that regulators are prioritizing immediate situational awareness upgrades for air traffic controllers. We view the $30 million targeted investment at EWR as a template the FAA is likely to replicate at other high-density hubs where legacy infrastructure limits operational capacity during low-visibility conditions.
Sources: Federal Aviation Administration
Photo Credit: Federal Aviation Administration
Regulations & Safety
FAA Revises Takeoff Obstacle Notes in Terminal Procedures
The FAA updates its Terminal Procedures Publication to simplify IFR departure planning with new DER crossing altitudes.

The Federal Aviation Administration (FAA) is revising the presentation of takeoff obstacle notes within its Terminal Procedures Publication (TPP), offering pilots a simplified method to utilize standard climb gradients during Instrument Flight Rules (IFR) departures.
In a press release issued on August 5, 2026, the National Business Aviation Association (NBAA) announced the charting updates. The revisions provide pilots with a specific Departure End of Runway (DER) crossing altitude, allowing them to safely clear low, close-in obstacles without calculating non-standard climb requirements for every individual threat.
Restructuring Obstacle Departure Procedures
Under the updated format, the FAA separates “Takeoff Minimums Obstacles” from “Low, Close-in Obstacles.” The agency defines low, close-in obstacles as those measuring 200 feet or less above the DER elevation.
Previously, pilots faced complex lists of individual obstacles during pre-flight planning. The new charting method consolidates these threats into distance groupings measured in quarter-mile increments from the DER. If a pilot meets the newly published DER crossing altitude, they can proceed using the standard IFR climb gradient of 200 feet per nautical mile (ft/NM) rather than a higher, non-standard gradient.
Industry advocacy and implementation timeline
The NBAA initially launched the effort to address the complexity of takeoff obstacle notes in 2015 during the FAA Aeronautical Charting Meeting. The resulting changes stem from collaboration between the FAA, the U.S. Instrument Flight Procedure Panel, and commercial charting providers including Jeppesen and Garmin.
While the FAA has officially adopted the new presentation standards, updating the entire National Airspace System will require a phased approach. The NBAA noted that the transition across all published procedures and commercial charts will take several years to complete.
AirPro News analysis
We view this charting revision as a practical step toward reducing pilot workload during IFR departure planning. By providing a clear DER crossing altitude that validates a standard 200 ft/NM climb, the FAA removes the ambiguity of evaluating multiple low, close-in obstacles individually. This change will be particularly beneficial for operators of aircraft with limited climb performance, allowing them to determine immediately if reported weather conditions permit visual obstacle avoidance when a higher climb gradient is unachievable.
Photo Credit: NBAA
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