Casualties unknown

2017-01-03: Saab-340A — Kijów (UKKK) / Warszawa (EPWA), PL

Kijów (UKKK) / Warszawa (EPWA), PL

On January 3, 2017, a Saab-340A was involved in an aviation accident near Kijów (UKKK) / Warszawa (EPWA), PL. Investigators recorded the probable cause as: Freezing of the control cables for the right engine power lever. 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 1785092869Data APIEditorial standards

During approach to Kyiv-Zhuliany, the crew of a SprintAir SAAB-340A found the right engine power lever stuck at cruise. Unable to reduce power, they shut down the engine and landed at Warsaw Chopin Airport.

Incident Overview

On January 3, 2017, a SAAB-340A aircraft operated by SprintAir S.A. experienced a power lever malfunction during flight. The crew was conducting an initial descent to land at Kyiv-Zhuliany Airport (UKKK) in Ukraine when they discovered that the right engine (No. 2) power lever was locked in the cruise power position and could not be moved. The decision was made to return to the home airport, Warsaw Chopin Airport (EPWA).

Crew Actions

Unable to reduce power on the right engine, the crew decided to shut it down. The engine was turned off at flight level 100. The aircraft then performed a single-engine landing on runway 33, which was executed normally. Prior to the shutdown, the crew consulted with the technical department regarding the procedure, as this specific scenario—shutting down an engine in flight with no capability to reduce power—was not covered in the Quick Reference Handbook (QRH).

Probable Cause

The investigation determined that the likely cause of the incident was freezing of the control cables for the right engine power lever.

Preventive Measures

Following the incident, SprintAir implemented several preventive actions: (1) Flight crew were briefed on the event and its circumstances. (2) A campaign was initiated to clean and dry the Condition Lever and Power Lever control cables on all fleet aircraft at the next convenient hangar maintenance opportunity. (3) To reduce recurrence risk, the drying interval for cables on SAAB-340 aircraft was reduced from 8 years to 2 years, to be performed concurrently with tasks 761108 and 761207 (Control Cable Tension Check). (4) The aircraft manufacturer was requested to amend the Abnormal Checklist in the QRH to include this scenario, as it was not covered by existing published procedures.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2017-0009/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.