Casualties unknown

2018-04-28: Bell Helicopter Textron 206L-4 (ZS-REG) — Farm Snymansdrift, East of Kuschke Nature Reserve, ZA

Farm Snymansdrift, East of Kuschke Nature Reserve, ZA

On April 28, 2018, a Bell Helicopter Textron 206L-4 (registration ZS-REG) was involved in an aviation accident near Farm Snymansdrift, East of Kuschke Nature Reserve, ZA. Investigators recorded the probable cause as: The primary cause of the accident was the **Loss of Tail Rotor Effectiveness (LTE)**, triggered by an abrupt right-hand maneuver at low airspeed and low altitude. This summary draws on records from the South African Civil Aviation Authority (SACAA) Accident and Incident Investigations Division.

Sourcesthe South African Civil Aviation Authority (SACAA) Accident and Incident Investigations DivisionPrimary reportUpdated 1785104676Data APIEditorial standards

A scenic flight over the Kuschke Nature Reserve ended in a crash after a Bell 206L-4 experienced an uncommanded yaw during a low-speed maneuver.

What happened

On 28 April 2018, a Bell 206L-4 helicopter, registration ZS-REG, was conducting a private scenic flight over the Kuschke Nature Reserve in Limpopo. The flight, which included the pilot and six passengers, was intended to view local wildlife. After approximately 15 minutes of low-level sightseeing, the pilot attempted to transition from a low-speed flight pattern to a right turn to return to the departure farm.

During this maneuver, the aircraft experienced a violent swing to the right, entering a spiral dive. The helicopter completed three full revolutions before impacting dense, bushy terrain. While the pilot attempted to regain control near the ground, the impact was unavoidable. The aircraft sustained severe damage, including the separation of the tail boom and the destruction of the skids. All seven occupants sustained minor injuries.

The investigation

SACAA AIID investigators examined the wreckage and flight parameters to determine the cause of the loss of control. The investigation confirmed that the aircraft was operating near its maximum all-up weight (MAUW) and was close to its center of gravity limits. Meteorological data indicated overcast conditions with mist present, which may have added to the pilot's workload.

Technical analysis of the wreckage showed that the engine was still producing power at the moment of impact. The investigation also reviewed the pilot's experience, noting that while the pilot held a valid license, they had only 41 hours of flight time specifically on this helicopter type.

Probable cause

The primary cause of the accident was the **Loss of Tail Rotor Effectiveness (LTE)**, triggered by an abrupt right-hand maneuver at low airspeed and low altitude. This maneuver caused the tail rotor to encounter airflow conditions that prevented it from maintaining directional control. Contributing factors included the aircraft operating near its maximum weight limits and the pilot's limited experience on this specific aircraft type.