Casualties unknown

2017-05-05: Bombardier DHC-8-Q400 (SP-EQE) — LJU, PL

LJU, PL

On May 5, 2017, a Bombardier DHC-8-Q400 (registration SP-EQE) was involved in an aviation accident near LJU, PL. Investigators recorded the probable cause as: The direct cause of the incident was the chafing of a hydraulic line. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL).

Sourcesthe Polish State Commission on Aircraft Accidents Investigation (PKBWL)Primary reportUpdated 1785697035Data APIEditorial standards
Aircraft registered SP-EQE
Aircraft registered SP-EQE. Photo: Aero Icarus from Zürich, Switzerland / CC BY-SA 2.0, via Wikimedia Commons

A hydraulic leak was discovered in the number two engine nacelle of a Bombardier DHC-8-402 during a pre-flight inspection at Ljubljana Airport.

What happened

On May 5, 2017, at approximately 14:50 UTC, the crew of a Bombardier DHC-8-402 was performing a pre-flight inspection at Ljubljana Airport (LJU) when they detected traces of hydraulic fluid leaking from the number two engine nacelle. Following an engine run test, the crew observed an increase in the leakage, prompting the cancellation of the scheduled flight.

Because the aircraft's operator did not have contracted maintenance services available at Ljubljana, a technical team was dispatched from Warsaw Chopin Airport (EPWA) to address the issue. Upon arrival, maintenance personnel inspected the engine nacelle and found that the hydraulic overflow bottles (ECO) were overfilled and identified two loose hydraulic line connections. The connections were tightened in accordance with the Aircraft Maintenance Manual (AMM), and the overflow bottles were cleaned. After passing a subsequent leak test, the aircraft was cleared to ferry to its home base.

However, upon arrival at EPWA, maintenance crews detected traces of hydraulic fluid leaking once again. To locate the source of the leak, technicians were required to remove the engine exhaust pipe. This inspection revealed a chafed hydraulic line located between the hydraulic fluid reservoir and hydraulic manifold number 2.

The investigation

The investigation focused on the sequence of maintenance actions and the physical condition of the hydraulic system components. The technical team examined the engine nacelle, the hydraulic line connections, and the area between the reservoir and the manifold to identify the source of the fluid loss.

Probable cause

The direct cause of the incident was the chafing of a hydraulic line.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2017-0813/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.