Casualties unknown

2018-06-10: Bombardier DHC-8-Q400 (SP-EQC) — Pilot samolotowy liniowy ATPL — TMA EPWA, PL

TMA EPWA, PL

On June 10, 2018, a Bombardier DHC-8-Q400 (registration SP-EQC) operated by Pilot samolotowy liniowy ATPL was involved in an aviation accident near TMA EPWA, PL. Investigators recorded the probable cause as: The incident was caused by a malfunction of the engine #2 oil cooler flap actuator. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 8 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
Aircraft registered SP-EQC
Aircraft registered SP-EQC. Photo: Alec Wilson from Khon Kaen, Thailand / CC BY-SA 2.0, via Wikimedia Commons

On June 10, 2018, a Bombardier DHC-8-402 departing Warsaw observed rising oil temperature on engine #2. The crew reduced power and returned to EPWA for a safe landing. The fault was traced to a stuck oil cooler flap actuator.

Incident Overview

On June 10, 2018, a Bombardier DHC-8-402 aircraft was conducting a scheduled flight from Warsaw (EPWA) to Budapest (LHBP). Shortly after takeoff, at approximately 14:10 UTC, the crew observed an increasing oil temperature on engine number 2. When the temperature reached 105°C (maximum allowable 107°C), the crew consulted the "HIGH OIL TEMPERATURE IN FLIGHT" checklist and reduced engine #2 power by 20%. This action lowered the oil temperature.

The aircraft's climb was stopped at flight level 100. The crew decided to return to EPWA and requested a holding pattern to burn off fuel and reduce landing weight. After consuming about 150 kg of fuel, the crew initiated an approach and landing, which was completed without further incident. The aircraft was then handed over to maintenance personnel. The crew submitted an Aircraft Safety Report (ASR).

Cause

The incident was caused by a malfunction of the engine #2 oil cooler flap actuator (ACOC FLAP ACTUATOR), part number 800600M03. Subsequent testing revealed that the actuator was stuck in the closed position, preventing proper oil cooling. The faulty actuator was replaced with a serviceable unit.

Safety Recommendations

No safety recommendations were issued by the investigation commission.

Probable cause

The incident was caused by a malfunction of the engine #2 oil cooler flap actuator.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2018-1499/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.