Jump to Content
Download Final Report
[ Download PDF: 11KB]
During take-off a pronounced thrust lever split was noticed. The N1 was split by 5% and, after manually adjusting the power levers, the pilot reported that the number 2 engine N1 and EGT rose rapidly above maximum limits. Thrust levers were retarded at 120 knots (V1 was 138 knots) and the take off was rejected. On the taxiway some smoke was seen coming from the tyres. An inspection showed that excessive lubrication of the landing gear brake units had caused the smoke when the brakes were overheated. No damage was evident. The number 2 engine was found to have sticky and out of adjustment variable stator vanes (VSV). These were lubricated and adjusted and subsequent operations were normal. Significant factors. 1. The pilot rejected the takeoff below V1 due to a power anomaly. 2. The number 2 engine variable stator vanes required adjustment and lubrication. 3.Excess lubrication on the landing gear brake units generated smoke after the rejected takeoff.
Download Final Report
[ Download PDF: 11KB]
General details
Date: 16 January 1993 Investigation status: Completed 
Time: 9:20 ESuT  
 Investigation type: Occurrence Investigation 
 Occurrence type: Abnormal engine indications 
Release date: 11 June 1993 Occurrence class: Technical 
Report status: Final Occurrence category: Incident 
Aircraft details
Aircraft manufacturer: The Boeing Company 
Aircraft model: 737-377 
Aircraft registration: VH-CZK 
Sector: Jet 
Damage to aircraft: Nil 
Departure point:Melbourne
Share this page Provide feedback on this investigation
Last update 23 July 2015