Casualties unknown

2019-03-29: Piper PA 30 (ZS-ICB) — Westonaria 16nm south-west of Johannesburg CBD, ZA

Westonaria 16nm south-west of Johannesburg CBD, ZA

On March 29, 2019, a Piper PA 30 (registration ZS-ICB) was involved in an aviation accident near Westonaria 16nm south-west of Johannesburg CBD, ZA. Investigators recorded the probable cause as: An incorrect throttle control cable end fitting was fitted to the aircraft’s right-side engine which separated on the third circuit as the student pilot applied full 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

On 29 March 2019, a Piper PA-30 (ZS-ICB) training flight crashed at Syferfontein Aerodrome after an incorrect throttle cable end fitting separated. The crew sustained minor injuries and the aircraft was destroyed.

History of Flight

On 29 March 2019, an instructor and a student pilot departed Rand Aerodrome (FAGM) for Syferfontein Aerodrome (FASY) to practice asymmetric circuits. After arrival, the instructor demonstrated the first asymmetric circuit on Runway 31 with a simulated right-engine failure. The student then took control for a second circuit. On downwind, the instructor simulated a left-engine failure. The student configured the aircraft for single-engine operation. On final approach at 300 feet AGL, the instructor restored power to the left engine, and the student landed successfully.

After touchdown, the student applied full power to both engines for takeoff. During rotation at about 80 knots, the aircraft banked sharply to the right. The instructor took control and attempted to feather the right engine, but it did not respond. The aircraft lost height, the right wing struck the ground, and the aircraft ground-looped and skidded to a stop 120 meters from Runway 14, facing opposite its takeoff direction.

Injuries and Damage

Both crew members sustained minor injuries. The aircraft was destroyed.

Investigation Findings

The investigation determined that an incorrect throttle control cable end fitting had been installed on the right engine. This fitting separated on the third circuit when the student pilot applied full power, preventing the engine from developing climb power and causing the right roll.

Probable cause

An incorrect throttle control cable end fitting was fitted to the aircraft’s right-side engine which separated on the third circuit as the student pilot applied full power.