Casualties unknown

2010-07-29: Robinson R22 Beta (ZS-RRM) — 5 nautical miles south of Panorama at GPS co-ordinates S26°23.680 E028°03.429, ZA

5 nautical miles south of Panorama at GPS co-ordinates S26°23.680 E028°03.429, ZA

On July 29, 2010, a Robinson R22 Beta (registration ZS-RRM) was involved in an aviation accident near 5 nautical miles south of Panorama at GPS co-ordinates S26°23.680 E028°03.429, ZA. Investigators recorded the probable cause as: Loss of control. Contributing factor: The corrective action by the pilot would have been to manually control the RPM first and then engage the governor, once stabilised. 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 private pilot experimenting with rotor RPM in a Robinson R22 caused an over-speed, lost situational awareness, and experienced a dynamic rollover. The helicopter was substantially damaged; the pilot was uninjured.

Accident Overview

On 29 July 2010, a Robinson R22 Beta helicopter, registration ZS-RRM, sustained substantial damage during a dynamic rollover while in a hover approximately 10 ft above ground. The accident occurred in the general flying area of Rand Aerodrome (FAGM), Gauteng Province, South Africa. The pilot, the sole occupant, was not injured.

History of Flight

The pilot departed Rand Aerodrome on a private flight. While maintaining a stable hover, he decided out of curiosity to test the effect of changing rotor and engine RPM on helicopter performance. He closed the throttle fractionally and then immediately opened it, causing an immediate increase in rotor and engine RPM, with the tachometer reading rising rapidly above the green arc. Focused on the instrument panel, the pilot lost situational awareness and failed to notice the helicopter banking to the right in a nose-down attitude. The right skid struck the ground, leading to a dynamic rollover onto the helicopter's right side. The pilot reported that he had attempted to fly with the governor off. The investigation determined the governor system was not defective but had been switched off.

Damage and Injuries

The helicopter sustained extensive damage. The pilot, properly restrained by safety belt and harnesses, suffered no injuries. No other persons were on board.

Probable Cause

The probable cause of the accident was loss of control. A contributing factor was that the pilot's corrective action would have been to manually control RPM first and then engage the governor once stabilised. The onset of the uncontrolled RPM profile alarmed the pilot and led to the incident.