Casualties unknown

2011-02-20: Enstrom 280 FX Helicopter (ZS-HWR) — Open stretch of veld on southern side of Kitty Hawk Aero Estate Airstrip, ZA

Open stretch of veld on southern side of Kitty Hawk Aero Estate Airstrip, ZA

On February 20, 2011, an Enstrom 280 FX Helicopter (registration ZS-HWR) was involved in an aviation accident near Open stretch of veld on southern side of Kitty Hawk Aero Estate Airstrip, ZA. Investigators recorded the probable cause as: The accident was caused by an unsuccessful autorotation landing following a sudden loss of engine power during flight, the specific cause of which could not be determined through engine testing. 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

An Enstrom 280 FX helicopter sustained substantial damage after an unsuccessful autorotation landing following a sudden loss of engine power.

What happened

On 20 February 2011, a private flight departing from Kitty Hawk Aero Estate Airfield experienced a sudden mechanical failure. While the pilot was increasing speed during takeoff, the engine began to splutter, which was immediately followed by a complete loss of power.

In response to the power loss, the pilot initiated an autorotation emergency landing procedure. An open area of veld south of the airfield was identified as a suitable landing site. As the Enstrom 280 FX approached the ground, the pilot attempted to flare the aircraft to cushion the impact. However, the landing was hard, causing the helicopter to strike the ground and roll onto its right side. The impact was severe enough that the main rotor blades struck the tail boom, severing the assembly and causing significant structural damage to the airframe, including the destruction of the skids, windscreen, and rotor components.

Despite the substantial damage to the aircraft, there were no injuries to the pilot or the passenger.

The investigation

SACAA AIID investigators examined the wreckage and the engine to identify the source of the power loss. A ground-run test was performed on the engine at various power settings, including maximum power, and the engine operated smoothly without any detectable anomalies.

Investigators also checked the fuel system for contamination. The right-hand fuel tank was found to be full, and testing revealed no signs of contaminated fuel. The left-hand tank was empty, having been depleted during the flight. The investigation confirmed that all aircraft documentation, including the Certificate of Airworthiness, was valid, and the helicopter had been maintained by an approved maintenance organization. The aircraft had undergone a mandatory periodic inspection only 0.6 hours prior to the accident.

Probable cause

The accident was caused by an unsuccessful autorotation landing following a sudden loss of engine power during flight, the specific cause of which could not be determined through engine testing.