Casualties unknown

2017-08-28: Bombardier DHC-8-Q400 (SP-EQH) — Pilot samolotowy liniowy ATPL — CTR WAW, PL

CTR WAW, PL

On August 28, 2017, a Bombardier DHC-8-Q400 (registration SP-EQH) operated by Pilot samolotowy liniowy ATPL was involved in an aviation accident near CTR WAW, PL. Investigators recorded the probable cause as: The cause of the incident was damage to the spring in the landing gear locking mechanism, which prevented correct retraction and locking of the right main landing gear and closure of the gear door. 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-EQH
Aircraft registered SP-EQH. Photo: Хомелка / CC BY-SA 4.0, via Wikimedia Commons

On August 28, 2017, a Bombardier DHC-8-Q400 experienced a right main landing gear door and lock indication issue after takeoff. The crew followed procedures and landed safely. A cracked spring was found in the locking mechanism.

Incident Overview

On August 28, 2017, at 15:10 UTC, shortly after takeoff from Warsaw Chopin Airport (EPWA) for a scheduled flight to Katowice (EPKT), the flight crew of a Bombardier DHC-8-Q400 observed two indicator lights illuminate during landing gear retraction. The amber "RIGHT MAIN GEAR DOOR NOT CLOSED" and red "RIGHT LANDING GEAR NOT LOCKED UP" warnings confirmed a problem with the right main landing gear.

Crew Actions

In response to the warnings, the crew immediately consulted the checklist and performed the alternate landing gear extension procedure. The aircraft returned to the departure airport, where an emergency landing was carried out without further incident.

Maintenance Findings

After landing, the aircraft was handed over to maintenance personnel. Inspection of the landing gear system revealed a cracked spring in the mechanism that locks the gear in the retracted position. This damage prevented the right main landing gear from retracting and locking properly, and also kept the gear door from closing.

Cause

The cause of the incident was damage to the spring in the landing gear locking mechanism, which prevented correct retraction and locking of the right main landing gear and closure of the gear door.

Post-Incident Actions

The operator recorded the event in its Safety Management System (SMS) database and classified it according to internal criteria. The incident was included in the operator's Safety Performance Indicators (SPIs), which are monitored as per the Safety Management Manual. No safety recommendations were issued by the investigation authority.

Probable cause

The cause of the incident was damage to the spring in the landing gear locking mechanism, which prevented correct retraction and locking of the right main landing gear and closure of the gear door.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2017-2314/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.