What happened
On the afternoon of 12 March 2026, a private flight departing from Mokopane Aerodrome (FAQR) in Limpopo Province ended in a fatal accident. The pilot was operating a Magni MTO Sport gyrocopter, registration ZU-RDP, for a local flight intended to return to the same airfield.
Earlier that morning, the aircraft had completed two previous flights during which the pilot experienced intense cockpit vibrations. The pilot launched this third flight specifically to investigate the source of these anomalies. Shortly after taking off from Runway 18 and climbing to approximately 300 feet, the aircraft performed two short left turns. During these maneuvers, one of the three main rotor blades detached from the rotor hub bar. The loss of the blade caused the pilot to lose control, leading the aircraft to crash into a field near the runway. The impact was so severe that the pilot was fatally injured, and the aircraft was destroyed.
The investigation
Investigators from the SACAA AIID examined the wreckage and the flight history of the aircraft. The investigation established that the aircraft was maintained by an approved person and had undergone a recent inspection in March 2026.
Physical examination of the wreckage revealed that the main rotor blade (serial number 1012) had snapped near the rotor hub bar. The detached section was located about 205 feet from the primary impact site. Analysis of the impact marks on the blade suggested that the detached component struck the right front section of the gyrocopter and the pilot's body during flight. Additionally, investigators noted ruptures in the rotor control linkage and damage at the connection point between the control fork and the rotor. Evidence from the propeller indicated that the engine was still producing significant power at the moment of impact.
Findings
- The primary cause of the accident was the in-flight separation of a main rotor blade.
- The pilot had experienced severe vibrations during two previous flights that morning, which had not been formally recorded in the flight folio.
- The aircraft's engine was producing substantial power at the time of the crash.
- The high-impact forces during the collision exceeded the limits of human physiological tolerance, rendering the accident non-survivable.