Incident Overview

Date: Sunday 19 August 2012
Aircraft Type: ATR 72-500 (72-212A)
Owner/operator: Flybe Nordic
Registration Number: OH-ATH
Location: Helsinki-Vantaa Airport (HEL/EFHK) – ÿ Finland
Phase of Flight: Landing
Status: Minor
Casualties: Fatalities: 0 / Occupants: 31
Component Affected: The rudder system, specifically the Travel Limitation Unit (TLU) actuator.The rudder system, specifically the Travel Limitation Unit (TLU) actuator.
Investigating Agency: SIAFSIAF
Category: Accident
A Finnish aircraft experienced a serious incident during landing due to a rudder control failure and a malfunction of the rudder?s Travel Limitation Unit (TLU). The rudder?s insufficient authority for directional control caused the aircraft to veer off the runway, resulting in a large directional oscillation. The incident was triggered by a broken TLU actuator, leaving it in HI SPD mode, and inadequate system awareness leading to the failure to activate the standby system.A Finnish aircraft experienced a serious incident during landing due to a rudder control failure and a malfunction of the rudder?s Travel Limitation Unit (TLU). The rudder?s insufficient authority for directional control caused the aircraft to veer off the runway, resulting in a large directional oscillation. The incident was triggered by a broken TLU actuator, leaving it in HI SPD mode, and inadequate system awareness leading to the failure to activate the standby system.

Description

Veered off the runway during landing following a rudder control failure. The Finnish Accident Investigation Board classified this as a serious incident and launched an investigation. Probable cause and consequence The serious incident was caused by the mechanically centred rudder?s insufficient authority for directional control, which resulted in the aircraft veering off the runway. Contributing factors The rudder?s Travel Limitation Unit (TLU) electric actuator broke and the TLU was left in the high speed (HI SPD) mode for the approach and landing, jamming the rudder. Due to inadequate system awareness and the fact that the QRH did not clearly enough provide instructions for using the TLU?s standby system, the flight crew did not switch on the TLU?s standby system. The right engine?s propeller blade angles transitioned sooner into the BETA zone following the reduction of engine power at landing, which resulted in a large directional oscillation.

Source of Information

http://www.turvallisuustutkinta.fi/Etusivu/Ajankohtaista/1342537306217, http://www.turvallisuustutkinta.fi/en/Etusivu/Ajankohtaista/Valmistuneettutkinnattiedotteet/1368802952710http://www.turvallisuustutkinta.fi/Etusivu/Ajankohtaista/1342537306217, http://www.turvallisuustutkinta.fi/en/Etusivu/Ajankohtaista/Valmistuneettutkinnattiedotteet/1368802952710

Primary Cause

Mechanically centred rudder?s insufficient authority for directional control, resulting in the aircraft veering off the runway.Mechanically centred rudder?s insufficient authority for directional control, resulting in the aircraft veering off the runway.

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