What happened
On June 26, 2016, a Bell 407 helicopter was performing a ferry flight from Assen, Netherlands, to Ingolstadt-Manching, Germany, with a planned refueling stop at Kassel-Calden. While flying near Hofgeismar, the pilot experienced torque fluctuations in the controls and a drop in the main rotor speed (Nr) to approximately 94%.
In response to the power loss, the pilot initiated an autorotation and selected a suitable field for an emergency landing. During the approach, the pilot successfully cleared an overhead power line. However, as the helicopter slid across a sloping field with high vegetation, the deceleration caused the aircraft to pitch forward. To prevent a forward tip-over, the pilot applied aft cyclic input, which caused the main rotor to strike the tail boom. The impact resulted in severe damage to the aircraft, including damage to the rotor head, the separation of the tail boom, and the loss of the tail rotor and vertical fins.
The pilot, who was highly experienced with over 5,00 and hours of total flight time, exited the aircraft uninjured. After the aircraft came to a stop, the pilot noted the engine was still running at reduced power and manually shut it down.
The investigation
The BFU investigation focused on the engine's Rolls-Royce M250-C47B turboshaft. While the engine's electronic control unit (ECU) did not record any hard faults or parameter exceedances—likely due to the pilot's rapid response—investigators found a damaged N2 speed sensor.
Upon disassembly of the engine, investigators identified significant damage to the No. 5 bearing. The investigation included a detailed analysis by the engine manufacturer in the United States. Findings revealed that the No. 5 bearing separator and several holding rings had fractured. Metal shavings were also discovered in the engine's chip detectors and oil filter.