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Shortly after take off an EICAS message 'flap Disagree' was indicated. The crew took appropriate action and the flight was continued. During climb out at FL205 a loud bang was heard accompanied by fluctuating right engine instrument indications and a yaw effect. The right engine was shut down and the aircraft returned to land at Melbourne. For the flap problem the recification consisted of replacement of the trailing edge flap bypass valve. For the engine malfunction the engine was changed. Significant Factors The following factors were considered relevant to the development of the incident: 1 Defective trailing edge bypass valve. 2 Right engine malfunction, reason undetermined.
Download Final Report
[ Download PDF: 11KB]
General details
Date: 25 January 1995 Investigation status: Completed 
Time: 15:10 ESuT  
 Investigation type: Occurrence Investigation 
 Occurrence type: Abnormal engine indications 
Release date: 16 May 1995 Occurrence class: Technical 
Report status: Final Occurrence category: Incident 
Aircraft details
Aircraft manufacturer: The Boeing Company 
Aircraft model: 767-238ER 
Aircraft registration: VH-EAO 
Sector: Jet 
Damage to aircraft: Nil 
Departure point:Melbourne VIC
Destination:Sydney NSW
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Last update 21 October 2014