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FAA investigating engine problems with Lycoming IO-360: Warning of possible engine rollbacks

Last updated on 18 January 2026
The US Federal Aviation Administration (FAA) has drawn attention to a potential safety issue with Lycoming IO-360 engines. Several incidents in which a sudden loss of power or even engine stoppage occurred when the throttle was released have triggered an official investigation. Numerous general aviation aircraft types are affected. The FAA is currently systematically collecting data from the field in order to narrow down the causes more precisely and develop suitable measures. The incident emphasises the importance of close cooperation between manufacturers, operators and authorities when it comes to the early detection of potential risks.

Background to the current FAA warning

The FAA has published an Airworthiness Concern Sheet (ACS) following several reports of unintended engine shutdowns on Lycoming IO-360 engines. These engines are among the most widely used four-cylinder engines in general aviation and are used in many training and touring aircraft.

According to previous findings, the problem often occurs during the transition to idle speed - for example during landing approaches, engine checks on the ground or when quickly reducing power. Pilots report so-called „rollbacks“, i.e. an abrupt drop in engine speed until the engine stalls.

Aircraft types and components affected

As things stand, the reports relate to IO-360 engines equipped with AVStar fuel servos. These servos are available in different variants and can be installed vertically or horizontally depending on the aircraft model. Rollback events have been observed with both types of installation.

The aircraft types that have been named so far include

  • Cessna 172S and 172R
  • Piper Archer III
  • Piper Pilot 100i
  • Piper Seminole

Since the IO-360 is installed in a large number of other models, the FAA expressly calls on all operators to report unusual engine behaviour - regardless of the manufacturer or the specific fuel control.

Possible technical backgrounds

Although the investigation is still ongoing, several technical aspects are being discussed as possible triggers:

  • Mixture preparation at extremely low engine speeds: The combination of servo calibration, carburettor pressure and constant speed control could result in the engine running too lean during rapid load changes.
  • Temperature and density conditions: Some reports indicate increased occurrence with warm engines or high ambient temperatures.
  • Tolerances between different servo variants: Differences in production or adjustment could favour individual deviations.
  • Transition behaviour in the throttle lever area: Some pilots report very short reaction windows in which the engine does not remain stable when the power is reduced quickly.

The FAA has not yet named any specific causes, as sufficient field reports are to be collected first.

Meaning of the Airworthiness Concern Sheet (ACS)

The ACS is an official instrument that is used before formal steps such as an Airworthiness Directive (AD) or a Mandatory Service Bulletin. The aim is to:

  • Collect information from the company
  • assess the relevance and frequency of a problem
  • Identify potential security risks at an early stage
  • involve the industry before binding measures are adopted

This procedure is particularly helpful if technical problems only occur sporadically or cannot yet be clearly localised.

Role of associations and type clubs

In general aviation, user organisations play an important role in safety communication. Organisations such as the Experimental Aircraft Association (EAA) and various type clubs have already called on pilots to report their experiences promptly. Their networks help to ensure that relevant information reaches the field quickly and that feedback from the field is collected comprehensively.

This support enables trends to be recognised early on and possible technical adjustments to be developed more quickly - such as changes to maintenance guidelines, servo settings or operating procedures.

What operators should do now

As long as the investigation is ongoing, owners, flight schools and maintenance companies are advised to pay increased attention:

  • Close observation of the idling behaviour for ground and flight tests
  • Checking the fuel servo settings as part of regular maintenance
  • Documentation of even minor anomalies, especially after rapid performance changes
  • Notification of all events via the contact point named in the ACS
  • Checking the engine and carburettor temperatures before the landing approach

Pilots should exercise particular caution during landing approaches and touch-and-go manoeuvres and, if in doubt, operate at slightly higher idle power until further information is available.

Outlook

The FAA now analyses all incoming data to determine whether technical or operational measures are necessary. Depending on the result, service bulletins, maintenance recommendations or - in the event of a significant safety risk - mandatory airworthiness directives could follow.

For general aviation, the case shows once again how important robust reporting chains and proactive communication are. By recognising patterns at an early stage, potential incidents can be prevented and safety maintained at a high level.


Source references:
Flieger.News

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