Engine failure during maneuver in Cabri G2 near Egelsbach

Casualties unknown • nahe Egelsbach, DE

A sudden engine failure occurred during a low-G maneuver in a Cabri G2 helicopter, leading to an emergency autorotation and subsequent investigation into carburetor defects.

What happened

On May 17, 2011, a Cabri G2 helicopter departed from the Frankfurt-Egelsbach airfield for a sightseeing flight accompanied by a passenger. While flying at approximately 1,500 ft AMSL, the pilot performed a "push over" maneuver involving reduced load factors. During this maneuver, the engine suddenly failed.

The pilot immediately initiated an autorotation and, after several attempts, successfully restarted the engine at approximately 50/500 ft GND. Following the restart, the pilot elected to return to Egelsbach. No further engine malfunctions or technical issues occurred during the remainder of the flight or the landing process. There were no fatalities and no damage to the aircraft or third parties.

The investigation

The BFU investigation focused on the cause of the engine failure and the subsequent series of engine failures observed during troubleshooting test flights. The investigation included an examination of the aircraft's Lycoming O-360-J2A engine and its Avstar MA-4SPA carburetor.

Following the initial incident, the operator performed extensive troubleshooting, which included replacing the carburetor multiple times and inspecting the electrical fuel pump and gascolator. The manufacturer also conducted test flights using different carburetors. These tests revealed that engine power loss and failures continued to occur specifically during low-G maneuvers (load factors below approximately 0.2 g), often accompanied by visible smoke.

Findings

Technical analysis of the carburetors revealed that the engine failure was caused by fuel overflow within the carburetor during maneuvers with low load factors.

Specifically, investigation of the original carburetor (S/N AV1127488) identified defects in the needle, needle seat, and float holder, which caused increased friction and impeded the movement of the float. A second carburetor (S/N AV11274416) was also found to suffer from leaks due to defects in the needle and needle seat area. These manufacturing or component defects allowed fuel to overflow at higher pressures/load changes, leading to the loss of engine power.

Probable cause

The engine failure was caused by fuel overflowing in the carburetor during low-G maneuvers due to mechanical defects in the needle, needle seat, and float holder, which restricted proper float movement.

Frequently asked questions

What happened in the 2011-05-17 Hélicoptères Guimbal Cabri G2 accident near nahe Egelsbach, DE?

A sudden engine failure occurred during a low-G maneuver in a Cabri G2 helicopter, leading to an emergency autorotation and subsequent investigation into carburetor defects.

What aircraft was involved and where did it happen?

The accident on 2011-05-17 involved a Hélicoptères Guimbal Cabri G2, at nahe Egelsbach, DE.

What was the probable cause of the accident?

The engine failure was caused by fuel overflowing in the carburetor during low-G maneuvers due to mechanical defects in the needle, needle seat, and float holder, which restricted proper float movement.

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