Casualties unknown

2020-05-03: CH 601 Zodiak (OK-JUA 80) — Pilot-uczeń — okolice EPPT, PL

okolice EPPT, PL

On May 3, 2020, a CH 601 Zodiak (registration OK-JUA 80) operated by Pilot-uczeń was involved in an aviation accident near okolice EPPT, PL. Investigators recorded the probable cause as: Interruption of power supply to the primary and backup engine injection and ignition control systems due to retraction of the connector in the switch plug for selecting these systems, leading to engine stoppage. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Polish State Commission on Aircraft Accidents Investigation (PKBWL)Primary reportUpdated 1785092869Data APIEditorial standards

On 3 May 2020, a student pilot experienced a sudden engine stoppage at 30-50 m altitude during a traffic pattern flight at Piotrków Trybunalski. A forced landing resulted in substantial damage, but the pilot was uninjured. The cause was a retracted electrical connector in the engine control switch.

Accident Summary

On 3 May 2020, at approximately 17:00 LMT, a student pilot (female) departed from runway 21 at Piotrków Trybunalski Airport (EPPT) in a CH601 ZODIAK aircraft (registration OK-JUA 80) for multiple traffic patterns. The first two circuits proceeded without issue.

Sequence of Events

Shortly after takeoff for the third circuit, at an altitude of 30–50 meters, the engine abruptly stopped. The pilot attempted to restart the engine and switched to the backup engine control system, but the engine did not restart. Facing low altitude and obstacles ahead, the pilot decided to execute a forced landing in a field to the right. The landing required a 90-degree turn, which was performed with excessive pitch and insufficient bank, resulting in a touchdown with sideways drift. The landing gear and engine cowling were damaged, and the aircraft struck a small embankment, causing the aircraft to pitch up, yaw, and eventually come to rest after a 180-degree rotation. No fuel leak or fire occurred. The aircraft sustained serious damage to the landing gear, propeller, engine mount, cowling, main frame, cabin structure, wingtip, and rear fuselage. The pilot was not injured. A police alcohol test was negative.

Investigation Findings

Examination of the engine revealed that a connector in the switch plug for selecting the primary and backup injection and ignition control systems had retracted from its proper position. The retracted connector interrupted power supply to both systems, causing the engine stoppage. The plug used standard 6.3 mm automotive connectors, which are secured by a bent tab; the tab may have deformed under the insertion force, allowing the connector to slip back.

Cause

The accident was caused by the interruption of power to the primary and backup engine injection and ignition control systems due to the retraction of a connector in the system selection switch plug, leading to engine stoppage.

Probable cause

Interruption of power supply to the primary and backup engine injection and ignition control systems due to retraction of the connector in the switch plug for selecting these systems, leading to engine stoppage.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2020-1155/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.