Casualties unknown

2008-10-27: Alouette II SNIAS SE3130 (ZU-RAH) — Helicopter landing area next to runway 20 at FABS, ZA

Helicopter landing area next to runway 20 at FABS, ZA

On October 27, 2008, an Alouette II SNIAS SE3130 (registration ZU-RAH) was involved in an aviation accident near Helicopter landing area next to runway 20 at FABS, ZA. Investigators recorded the probable cause as: Pilot lost control of the aircraft during adverse wind conditions. 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 student pilot on his third solo circuit lost control of an Alouette II helicopter while hovering, leading to a hard landing and rollover. The pilot sustained minor injuries and the aircraft was substantially damaged.

History of Flight

On 27 October 2008 at 1610Z, a student pilot was conducting his third solo circuit training flight at Brits Aerodrome in an Alouette II helicopter (registration ZU-RAH). The pilot approached the concrete block landing area next to runway 20 and positioned the helicopter into a hover approximately 3 meters above the ground. After a short period, the helicopter began to turn left on its vertical axis. The first 180 degrees of the turn were erratic, and then the helicopter spun excessively to the left for about 20 seconds. During this spin, the helicopter gained approximately 2 meters in height before moving toward the eastern side of the runway and descending.

Injuries and Damage

The helicopter landed hard in an upright position on its skids but rolled onto its right-hand side moments later, causing the main rotor blades to strike the ground. The pilot exited the helicopter, then re-entered to shut off the running engine before exiting again. He was transported by NETCARE 911 to a hospital for observation and sustained only minor injuries. The helicopter sustained substantial damage to the fuselage, main rotor blades, tail rotor, landing skids, and airframe. No other damage occurred on the ground.

Probable Cause

The probable cause is that the pilot lost control of the aircraft during adverse wind conditions.