Casualties unknown

2018 Robinson R44 Raven II Accident in South Africa (ZS-MZS)

Lumarie Game Farm, ZA

On June 1, 2018, a Robinson R44 Raven II (registration ZS-MZS) was involved in an aviation accident near Lumarie Game Farm, ZA. Investigators recorded the probable cause as: It is probable that during forward movement, the helicopter entered a transverse flow effect which resulted in the helicopter rolling to the right. 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 2026-09-13Data APIEditorial standards

On 1 June 2018, a Robinson R44 Raven II (ZS-MZS) crashed in Limpopo, South Africa, killing the pilot and passenger. The aircraft was destroyed without fire.

Accident Overview and Flight Details On 1 June 2018, a Robinson R44 Raven II helicopter, registration ZS-MZS, was destroyed in a crash in South Africa. The aircraft, operated by Marico Hill Game Lodge (Pty) Ltd, departed Rustenburg Aerodrome (FARG) in the North West Province at approximately 0900Z for a private flight under visual flight rules. The intended destination was Zebula Golf Estate & Spa Aerodrome in Limpopo Province. The accident occurred at 0940Z at Lumarie Game Farm, located 8 nautical miles south-west of the destination aerodrome. The site was at GPS coordinates S24°52’07.71” E027°52’27.97” with an elevation of 3,920 feet. ## Personnel and Aircraft Information The helicopter carried two occupants: a 36-year-old male pilot-in-command and one passenger. Both were fatally injured. The pilot held a valid Private Pilot Licence (Helicopter) and had a total of 406.8 flying hours, including 68.6 hours on the Robinson R44 type. The aircraft, serial number 12180, was manufactured on 20 February 2008 and had 653.6 total airframe hours at the time of the accident. ## Accident Sequence and Investigation Eyewitnesses near Quinta Domingo Farm gate observed the helicopter approaching from the south. It hovered at a low height of less than 150 feet above ground level before moving forward, losing height, and making a left turn. The helicopter then rolled to the left and crashed in a nose-down attitude. A main rotor blade separated during the sequence, damaging a perimeter fence. There was no pre- or post-impact fire. The investigation noted a possible debonding of the blade skin from a main rotor spar, which could have caused destabilization, though this was not conclusively proven. It was probable that the helicopter entered a transverse flow effect during forward movement, causing a roll to the right. The pilot's overcompensation with the cyclic control to the left resulted in a loss of control and the subsequent crash.

Probable cause

It is probable that during forward movement, the helicopter entered a transverse flow effect which resulted in the helicopter rolling to the right. To correct the roll, the pilot moved the cyclic control to the left but he over compensated, resulting in the loss of control and the subsequent crash.