Casualties unknown

2002-07-05: Jabiru SP (ZU-SES) — Ellisras Aerodrom, ZA

Ellisras Aerodrom, ZA

On July 5, 2002, a Jabiru SP (registration ZU-SES) was involved in an aviation accident near Ellisras Aerodrom, ZA. Investigators recorded the probable cause as: After landing it was not possible to rotate the engine and a tear down inspection was conducted, where it was found that the No. 3 cylinder-exhaust valve had failed in fatigue. 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 5 July 2002, a Jabiru SP (ZU-SES) experienced sudden engine roughness and partial power loss during a commercial survey flight. The pilot aborted the mission and landed safely at Ellisras Aerodrome. Post-flight examination revealed a fatigue failure of the No. 3 cylinder exhaust valve, leading to engine seizure. No injuries were reported.

Incident Overview

On 5 July 2002, at 1024Z, a Jabiru SP aircraft, registration ZU-SES, was engaged in a commercial geographical survey flight departing from and returning to Ellisras Aerodrome. The weather was reported as fine. The aircraft carried one person on board.

Sequence of Events

During the flight, the engine suddenly started running rough, accompanied by a partial loss of engine power. The engine oil temperature began to increase, and the pilot detected a smell of hot metal. Consequently, the survey flight was abandoned, and the pilot decided to return to Ellisras Aerodrome, where a safe landing was executed.

After shutdown, an attempt was made to rotate the engine by turning the propeller, but it was not possible. The assistance of an Aircraft Maintenance Engineer (AME) was called in, as the engine appeared to have seized during operation.

Investigation Findings

A tear-down inspection was conducted. It was found that the No. 3 cylinder exhaust valve had failed in fatigue. This failure resulted in secondary internal engine damage, followed by a subsequent engine seizure. No injuries or fatalities were reported.

Probable cause

After landing it was not possible to rotate the engine and a tear down inspection was conducted, where it was found that the No. 3 cylinder-exhaust valve had failed in fatigue. This resulted in secondary internal engine damage followed by a subsequent engine seizure.