No fatalities

LPR Lublin EC 135 P2+ Incident: TQ Exceedances During HEMS Flight (SP-HXC)

EPLR, PL

On March 10, 2017, an EUROCOPTER, EC-135 (registration SP-HXC) was involved in an aviation accident near EPLR, PL. No fatalities were reported. Investigators recorded the probable cause as: Improper distribution of attention during the final phase of the helicopter's acceleration. 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 2026-10-18Data APIEditorial standards
Aircraft registered SP-HXC
Aircraft registered SP-HXC. Photo: Faxe / CC BY-SA 3.0, via Wikimedia Commons

On 9 March 2017, an LPR Lublin EC 135 P2+ completed a HEMS flight to Tarnawka. Post-flight UMS/PGS review revealed torque exceedances on both engines, requiring Category B maintenance within five hours.

Incident Overview and Flight Details On 9 March 2017, the crew of the Lublin branch of the Polish Air Rescue Service (LPR) conducted a HEMS flight to Tarnawka in an EC 135 P2+ helicopter. The mission was carried out and completed without operational consequences. The event was recorded by the State Commission for Investigation of Aviation Accidents (PAŃSTWOWA KOMISJA BADANIA WYPADKÓW LOTNICZYCH) under incident number 389/17 and classified as an incident. ## Post-Flight Findings Following the flight, the crew reviewed records from the UMS/PGS system, which logs exceedances. The review identified torque (TQ) exceedances on both engines during the flight. On the left engine, designated as number 1, the maximum TQ reached 70.2% for 10.75 seconds. On the right engine, designated as number 2, the TQ reached 70.8% for 10.75 seconds. The crew did not observe these exceedances during the operation. ## Maintenance Actions In accordance with MSM 05-51-00, 6-8, the identified exceedances required Category B maintenance within the next five hours of helicopter operation. The required tasks included washing the main gearbox oil filter, inspecting the main and final gearbox chip detectors, and inspecting the main rotor hub. All tasks were completed within the prescribed time, and the helicopter was found to be serviceable. ## Probable Cause and Follow-Up The probable cause of the incident was identified as improper distribution of attention during the final phase of the helicopter's acceleration. The event was discussed with all LPR operational personnel as a preventive measure. The Commission did not formulate safety recommendations.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2017-0389/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.