Incident Overview

Date: Saturday 21 January 1989
Aircraft Type: Swearingen SA226-TC Metro II
Owner/operator: Muk Air Taxi
Registration Number: OY-ARI
Location: ™rnsk”ldsvik Airport (OER) – ÿ Sweden
Phase of Flight: Landing
Status: Destroyed, written off
Casualties: Fatalities: 0 / Occupants: 17
Component Affected: PropellerPropeller
Investigating Agency: SHKSHK
Category: Accident
On a climbing flight at 7000 feet, the no. 1 engine experienced a low oil pressure warning light. Upon engine stop, a fuse blew, disabling the right side instruments lights. The crew returned to the airport and performed an ILS approach, with rudder and elevator fully deflected. The aircraft touched down 30 meters left of the runway. The probable cause was a misrigged feathering handle resulting in drag, which the pilot was unable to compensate with trim and rudder, leading to the aircraft landing on the side of the runway.On a climbing flight at 7000 feet, the no. 1 engine experienced a low oil pressure warning light. Upon engine stop, a fuse blew, disabling the right side instruments lights. The crew returned to the airport and performed an ILS approach, with rudder and elevator fully deflected. The aircraft touched down 30 meters left of the runway. The probable cause was a misrigged feathering handle resulting in drag, which the pilot was unable to compensate with trim and rudder, leading to the aircraft landing on the side of the runway.

Description

The no. 1 engine low oil pressure warning light came on while climbing through 7000 feet. When the engine was stopped, a fuse blew and only the right side instruments lights functioned. The crew returned to the airport and preformed an ILS approach. The prop hadn’t feathered so rudder and elevator were fully deflected. The aircraft touched down 30 m left of the runway. Probable cause: (translated from Swedish) Due to the fact that left propeller did not go to feathering mode, a drag arose which the pilot could not compensate with trim and rudder, so that the aircraft landed on the side of the runway. Contributing factors: – Oil leakage in the engine which made it necessary to stop the left engine and feather the propeller. – Power supply problems caused by the left side not having been isolated from the right side. – A misrigged feathering handle – Inadequate checklists.

Primary Cause

Misrigged feathering handle leading to drag and loss of control.Misrigged feathering handle leading to drag and loss of control.

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