Engine power loss leads to forced landing of Tecnam P96 Golf in North West Province

Casualties unknown • Bâle-Mulhouse Aéroport (LFSB)/FRA, CH

A private flight experienced engine power loss due to low fuel pressure, forcing the pilot to perform an emergency landing on a gravel road near Brui.

What happened

On 5 July 2024, a Tecnam P96 Golf, registration ZU-DLU, was conducting a private flight from Sishen Airport in the Northern Cape to a destination near Brui in the North West Province. The flight was operating under Visual Meteorological Conditions (VMC) in accordance with Part 94 regulations.

Approximately ten minutes after departure, while cruising over a remote area near Brui, the pilot observed a low fuel pressure warning. Shortly thereafter, the engine lost power. The pilot successfully identified a gravel road adjacent to the R379 and executed a forced landing. During the touchdown on the uneven, shrub-filled surface, the aircraft sustained minor damage to the left wing, left elevator, and the underside of the fuselage. The pilot escaped the incident without injury.

The investigation

SACAA AIID investigators examined the engine and fuel system following the incident. Post-accident testing of the engine showed no mechanical defects, and the engine met all required operating parameters during subsequent runs. The fuel on board was found to be of the correct grade, sufficient in quantity, and free of contaminants. No disconnections were found in the carburettors or throttle control.

An assessment of the fuel system design noted the absence of an overflow fuel return line. Investigators considered that the lack of this component might lead to induced fuel vapor lock caused by engine heat during operations in high-temperature environments, such as those found in South Africa.

Findings

  • The pilot held a valid Private Pilot Licence and a current Class 2 medical certificate.
  • The aircraft had a valid Authority-to-fly and a current Certificate of Release to Service.
  • No mechanical defects or fuel restrictions were identified during post-incident engine testing.
  • The aircraft's European design may be susceptible to technical issues when operating in extreme heat due to the lack of a fuel return line, potentially causing vapor lock.

Probable cause

The exact cause of the engine power loss remains undetermined, though the absence of a fuel return line may have contributed to fuel vapor lock under high heat.

Frequently asked questions

What happened in the 1965-05-02 PIPER AIRCRAFT CORPORATION J3C-65/L-4. accident near Bâle-Mulhouse Aéroport (LFSB)/FRA, CH?

A private flight experienced engine power loss due to low fuel pressure, forcing the pilot to perform an emergency landing on a gravel road near Brui.

What aircraft was involved and where did it happen?

The accident on 1965-05-02 involved a PIPER AIRCRAFT CORPORATION J3C-65/L-4., registration HB-ORO, at Bâle-Mulhouse Aéroport (LFSB)/FRA, CH.

What was the probable cause of the accident?

The exact cause of the engine power loss remains undetermined, though the absence of a fuel return line may have contributed to fuel vapor lock under high heat.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/233.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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