Incident Overview

Date: Friday 7 October 2005
Aircraft Type: de Havilland Canada DHC-8-311Q Dash 8
Owner/operator: British Airways Citiexpress
Registration Number: G-BRYW
Location: Aberdeen-Dyce Airport (ABZ) – ÿ United Kingdom
Phase of Flight: Standing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 54
Component Affected: Right propeller blades, fuselage, and forward-neutral-reverse selector.Right propeller blades, fuselage, and forward-neutral-reverse selector.
Investigating Agency: AAIBAAIB
Category: Accident
A DHC-8 aircraft experienced a mechanical failure during parking at Aberdeen Airport. Following the disconnection of GPU cables, a ground power unit moved forward, striking the right propeller, resulting in significant damage to the propeller and fuselage. The incident was caused by a combination of three mechanical defects: a worn ball joint on the governor rod, a worn fuel pump spring, and a worn gate in the forward-neutral-reverse selector. These defects were identified as stemming from inadequate maintenance practices and a lack of appropriate servicing schedule adherence.A DHC-8 aircraft experienced a mechanical failure during parking at Aberdeen Airport. Following the disconnection of GPU cables, a ground power unit moved forward, striking the right propeller, resulting in significant damage to the propeller and fuselage. The incident was caused by a combination of three mechanical defects: a worn ball joint on the governor rod, a worn fuel pump spring, and a worn gate in the forward-neutral-reverse selector. These defects were identified as stemming from inadequate maintenance practices and a lack of appropriate servicing schedule adherence.

Description

The DHC-8 aircraft was parked on Stand 8 at Aberdeen Airport, U.K. All the passengers were on board and the engines had been started. Shortly after the Ground Power Unit (GPU) cables had been disconnected from the aircraft, and with nobody in the cab, the GPU moved forward and struck the rotating propeller on the right engine before coming to rest against the fuselage. All the occupants exited the aircraft through the passenger door and no one was injured. The right propeller had suffered significant damage to all four blades and to its hub. The right engine had come to an abrupt halt and, as a result, the engine required a complete overhaul. Also, there was a dent in the fuselage with associated local damage to the fuselage structure. Conclusions: The incident occurred because the GPU was being operated with a worn ball joint on the governor rod, a worn fuel pump spring and a worn gate in the forward-neutral-reverse selector. These three mechanical defects are attributed to: a) Inadequacies in the operator’s maintenance system, including defect reporting. b) The lack of appropriate checks in the manufacturer’s recommended servicing schedule

Primary Cause

Inadequate maintenance practices, specifically the presence of worn ball joint, fuel pump spring, and gate selector, leading to mechanical failures.Inadequate maintenance practices, specifically the presence of worn ball joint, fuel pump spring, and gate selector, leading to mechanical failures.

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