Casualties unknown

2013-06-24: Airbus A330-243 (G-OMYT ) — Manchester Airport, GB

Manchester Airport, GB

On June 24, 2013, an Airbus A330-243 (registration G-OMYT) was involved in an aviation accident near Manchester Airport, GB. Investigators recorded the probable cause as: The failure of the HP turbine blade was caused by high cycle fatigue propagation due to surface damage as a result of Type 2 Sulphidation corrosion. This summary draws on records from the UK Air Accidents Investigation Branch (AAIB); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe UK Air Accidents Investigation Branch (AAIB)Primary reportUpdated 1785053200Data APIEditorial standards
Aircraft registered G-OMYT
Aircraft registered G-OMYT . Photo: Craig Sunter from Manchester, UK / CC BY 2.0, via Wikimedia Commons

Forensic analysis of an HP turbine blade failure on an Airbus A330-243 at Manchester Airport determined the cause to be high cycle fatigue from Type 2 Sulphidation corrosion. No volcanic origin was found for surface deposits.

Incident Overview

On 24 June 2013, an Airbus A330-243, registration G-OMYT, experienced a high-pressure (HP) turbine blade failure at Manchester Airport. The incident was investigated by the engine manufacturer, and a forensic report was issued.

Blade Failure Analysis

Examination revealed that the blade failure resulted from high cycle fatigue propagation, which was attributed to surface damage caused by Type 2 Sulphidation corrosion. During the investigation, unidentified deposits were found on the blade surfaces, raising concern that they might be volcanic in origin, specifically from the 2010 eruption of Eyjafjallajökull in Iceland.

Additional Forensic Testing

Further forensic analysis was conducted to determine the composition of the deposits. Completed in August 2014, the analysis did not identify compounds typically associated with volcanic activity. While an encounter with volcanic gaseous sulphur could not be entirely discounted, the investigation concluded that the deposits were probably an accumulation of atmospheric dirt and pollutants.

Probable cause

The failure of the HP turbine blade was caused by high cycle fatigue propagation due to surface damage as a result of Type 2 Sulphidation corrosion.