Casualties unknown

2000-09-10: Beech F33A (ZS-MRM) — km from threshold of Runway 35 (FALA)., ZA

km from threshold of Runway 35 (FALA)., ZA

On September 10, 2000, a Beech F33A (registration ZS-MRM) was involved in an aviation accident near km from threshold of Runway 35 (FALA)., ZA. Investigators recorded the probable cause as: The engine failure was likely caused by an excessively lean fuel/air mixture, which resulted in the engine's inability to maintain necessary power. 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 Beech F33A experienced a sudden loss of engine power during its approach to Lanseria, resulting in an emergency forced landing in an open field.

What happened

On 10 September 2000, a Beech F33A, registration ZS-MRM, was conducting a private flight from Gaborone, Botswana, to Lanseria, South Africa. The aircraft was carrying a pilot and three passengers. While the aircraft was positioned on a right downwind leg for Runway 35 at Lanseria, at an altitude of approximately 5,500 feet, the pilot experienced a sudden loss of engine power.

Following the engine failure, the pilot initiated standard emergency procedures and notified the control tower of the situation. As the aircraft began a rapid descent, the decision was made to perform a forced landing. The aircraft impacted an open field located roughly 1 km from the threshold of Runway 35. The aircraft came to a complete stop approximately 50 meters from the initial point of impact. There were no injuries reported among the four occupants.

The investigation

The investigation focused on the circumstances surrounding the engine's failure to maintain power during the approach phase. Investigators examined the flight path, the pilot's response to the emergency, and the mechanical state of the engine during the descent.

Probable cause

The engine failure was likely caused by an excessively lean fuel/air mixture, which resulted in the engine's inability to maintain necessary power.