Aviation safety investigations & reports

Engine failure involving Airbus A380, A6-EDA near Sydney Airport, NSW, 11 November 2012

Investigation number:
Status: Completed
Investigation completed


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What happened

On 11 November 2012, an Emirates A380 aircraft, registered A6-EDA, departed Sydney Airport for Dubai, United Arab Emirates. While climbing through an altitude of approximately 9,000 ft, the crew reported hearing a loud bang, accompanied by an engine No 3 exhaust gas temperature over-limit warning. Shortly thereafter, the engine went through an uncommanded shut down. The crew jettisoned excess fuel and returned the aircraft to Sydney for a safe landing and disembarkation of the passengers and crew.

What the ATSB found

The investigation found that the increase in the exhaust gas temperature and subsequent engine shut down was a result of significant internal damage that had initiated within the high pressure turbine (HPT) module. The damage had resulted from the effects of HPT stage-2 nozzle distress, likely caused by exposure to hotter than expected operating temperatures. The nozzle distress led to eventual failure and separation into the gas flowpath. Over the preceding weeks there were two other engines within the operator’s fleet that had experienced a similar problem, and a number of steps had been taken by the manufacturer to address the issue, including the increased monitoring of distress development. During the previous flight, the engine health and trend monitoring program had identified a performance trend shift with this particular engine, and it was due to be inspected upon return to the main base in Dubai.

What's been done as a result

The engine manufacturer, Engine Alliance, had issued a service bulletin in June 2010 for the replacement of affected HPT stage-2 nozzle segments with new, more durable components during the next workshop visit when the HPT stage-2 was removed from the engine. Following this occurrence, another service bulletin was released on 6 December 2012, requiring the direct inspection of the nozzle segments that had not yet been replaced. The US Federal Aviation Administration also released an Airworthiness Directive which required inspection of the nozzle segments and their removal from service if distress was identified.

As the nozzle degradation mechanism was an emerging issue for the engine manufacturer at the time of the occurrence, the information and experiences associated with this occurrence have been used to refine and improve the trend monitoring program. Under the new limits set, this engine would have been inspected two flights prior to the occurrence flight. At the time this report was released, the manufacturer was continuing work to better understand the initial onset of nozzle distress and potential for further design improvements.

Safety message

While the distress to the HPT was severe enough in this case to result in an in-flight engine shutdown, the associated risks to the safety of continued flight were relatively low, given the failure had been contained and the operator’s procedures were effective in managing the engine shut down. This occurrence also pointed to the value of real-time engine condition monitoring, since advanced warning of engine degradation and efficiency loss allows inspection and corrective action before damage progresses to a level where it can cause an in-flight shut down.

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Safety Issues

Go to AO-2012-150-SI-01 - Go to AO-2012-150-SI-02 -

High pressure turbine stage-2 nozzle distress

The design cooling characteristics of the Engine Alliance GP7200 high pressure turbine (HPT) stage-2 nozzle components led to higher than expected metal surface temperatures during operation, rendering the nozzles susceptible to distress, premature degradation and failure.

Safety issue details
Issue number: AO-2012-150-SI-01
Who it affects: All operators of A380 aircraft with Engine Alliance GP7200 engines fitted
Status: Adequately addressed

Engine trend monitoring limits

The threshold limits for the engine trend monitoring program were not set at a level that provided sufficient opportunity for inspection of the engine before failure could occur from the effects of HPT stage-2 nozzle degradation.

Safety issue details
Issue number: AO-2012-150-SI-02
Who it affects: All operators of A380 aircraft with Engine Alliance GP7200 engines fitted
Status: Adequately addressed
General details
Date: 11 November 2012   Investigation status: Completed  
Time: 2205 ESuT   Investigation level: Defined - click for an explanation of investigation levels  
Location   (show map): near Sydney Airport    
State: New South Wales   Occurrence type: Engine failure or malfunction  
Release date: 09 September 2013   Occurrence category: Incident  
Report status: Final   Highest injury level: None  

Aircraft details

Aircraft details
Aircraft manufacturer Airbus Industrie  
Aircraft model A380  
Aircraft registration A6-EDA  
Serial number 11  
Operator Emirates Airlines  
Type of operation Air Transport High Capacity  
Damage to aircraft Minor  
Departure point Sydney NSW  
Destination Dubai UAE  
Last update 14 November 2018