Casualties unknown

2002-03-18: Hughes 269 C (ZS-HVD) — Farm Doornlaagte in the Northern Cape, ZA

Farm Doornlaagte in the Northern Cape, ZA

On March 18, 2002, a Hughes 269 C (registration ZS-HVD) was involved in an aviation accident near Farm Doornlaagte in the Northern Cape, ZA. Investigators recorded the probable cause as: The loss of engine power and subsequent engine failure could be attributed to the seizure of the No. 3 connecting rod big-end bearing. It is considered that the failure was a result of restricted oil flow over a period to the big-end bearing. 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 1785709791Data APIEditorial standards

A Hughes 269C experienced engine power loss shortly after takeoff, leading to a forced landing in wooded terrain. The main rotor RPM decayed, resulting in a hard landing that severed the tail boom. No injuries occurred.

Summary

On March 18, 2002, at approximately 1030Z, a Hughes 269C helicopter (registration ZS-HVD) departed from Farm Doornlaagte near Deben in the Northern Cape, South Africa, on a private flight with one pilot and one passenger. Shortly after takeoff, the aircraft experienced a loss of engine power followed by a complete engine failure. The pilot executed a forced landing in a densely wooded area.

Accident Details

During the forced landing, the pilot attempted to select a suitable landing area but allowed the main rotor RPM to decay substantially. The helicopter subsequently made a hard landing. The impact caused the rear cross tube assembly to fail, allowing the main rotor blades to sever the tail boom. The aircraft was substantially damaged, but nobody on board was injured. Meteorological conditions at the time were reported as fine.

Probable Cause

The loss of engine power and subsequent engine failure were attributed to the seizure of the No. 3 connecting rod big-end bearing. It is considered that the failure resulted from restricted oil flow over a period to the big-end bearing.