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During cruise the pilot noticed that the electrical system was malfunctioning. The ammeter was reading zero, the system was switched off and a diversion for landing carried out. The pilot reported that, on arrival in the circuit area, the landing gear could not be lowered by the emergency system. A wheels-up landing was made. An inspection of the aircraft revealed that the electrical problems were due an alternator failure which resulted from a faulty connection on a brush lead. The reason that the gear was unable to be lowered by the emergency system could not be determined.

Download Final Report
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General details
Date: 04 July 1984 Investigation status: Completed 
Time: 1421 Investigation type: Occurrence Investigation 
Location:Charleville Occurrence type:Wheels up landing 
State: Queensland Occurrence class: Operational 
Release date: 23 December 1985 Occurrence category: Accident 
Report status: Final Highest injury level: None 
 
Aircraft details
Aircraft manufacturer: Piper Aircraft Corp 
Aircraft model: PA-32 
Aircraft registration: VH-SBK 
Type of operation: Charter 
Damage to aircraft: Substantial 
Departure point:Roma QLD
Departure time:U/K
Destination:Windorah QLD
 
 
 
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Last update 13 May 2014