Casualties unknown

Engine Failure and Forced Landing of Robinson R44 II near Nelspruit (ZS-RSO)

Private farm Rocky Drift, Mpumalanga, ZA

On January 14, 2014, a Robinson R44 II (registration ZS-RSO) was involved in an aviation accident near Private farm Rocky Drift, Mpumalanga, ZA. Investigators recorded the probable cause as: Successful forced landing following an engine stoppage or failure during flight. Contributory factors: Connecting rod failure. Oil supply failure which caused oil pressure drop. 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

A Robinson R44 II helicopter experienced a sudden engine power loss during a private flight near Nelspruit, South Africa. The pilot performed an autorotation and landed safely. No injuries or damage occurred. Investigation revealed a connecting rod failure.

Incident Overview

On 14 January 2014, a Robinson R44 II helicopter, registration ZS-RSO, was conducting a private flight in the Nelspruit area. The helicopter lost engine power within three seconds, accompanied by moderate to severe vibrations. The manifold pressure indicator increased above 25 inches, while oil pressure dropped to the red line, followed by a sudden engine stoppage. The pilot initiated an autorotation, identified a landing strip, and landed the helicopter safely. No occupants were injured, and the helicopter sustained no damage.

Aircraft and Personnel

The helicopter was a Robinson R44 II (serial number 10145), manufactured in 2003, with a total airframe time of 1,675.6 hours. The engine was a Lycoming IO-540-AE1A5 (serial L-32118-48A) with 470.4 hours since new and 48.7 hours since overhaul. The pilot, aged 22, held a private pilot licence with 161.2 total flying hours, including 60.0 hours on type. The flight was private, with one passenger on board.

Meteorological Conditions

Weather at the time was reported as CAVOK, with surface wind light and variable at 315°, temperature 25°C, and clear skies. Visibility was clear.

Investigation Findings

The helicopter was transported to an approved maintenance organization for examination. Visual inspection of the engine revealed no external leaks or damage. The affected connecting rod bushing had failed, resulting in a connecting rod failure and damage to the bottom of the engine casing. Metal particles were found in the oil sump. The investigation established that due to the fact that the connecting rod converts the pistons reciprocating motion into the rotational motion of the crankshaft, the failure could be attributed to undetermined overload during such conversion. Additionally, oil supply failure caused a drop in oil pressure.

Probable Cause and Contributing Factors

The probable cause of the incident was a successful forced landing following an engine stoppage or failure during flight. Contributing factors were connecting rod failure and oil supply failure, which caused a drop in oil pressure.