Jump to Content
Download Final Report
[ Download PDF: 12KB]
The pilot reported that the aircraft engine lost power when he made a power adjustment whilst on final approach. The propeller feathered and the aircraft landed short of the runway on unprepared ground, incurring substantial damage. The aircraft was being used for parachute drops from 14,000ft. When the last parachutist left the aircraft, the pilot would place the aircraft in a steep spiralling descent. During this type of descent, the pilot was known to exceed the 60 degree angle of bank limits for the aircraft. Low fuel states were reported as being used for the paradrops. It is probable that the fuel flow from the wing cells to the collector tank (18 litre capacity) was interrupted during the descent and air entered the system. The fuel pump was not designed to operate in other than a full collector tank. As a result it is likely that the fuel flow to the engine was interrupted, resulting in engine flame out.
Download Final Report
[ Download PDF: 12KB]
General details
Date: 08 January 1995 Investigation status: Completed 
 Investigation type: Occurrence Investigation 
 Occurrence type: Fuel starvation 
Release date: 05 June 1996 Occurrence class: Operational 
Report status: Final Occurrence category: Accident 
Aircraft details
Aircraft manufacturer: Cessna Aircraft Company 
Aircraft model: 208 
Aircraft registration: VH-MMV 
Sector: Turboprop 
Damage to aircraft: Substantial 
Departure point:Toogoolawah QLD
Destination:Toogoolawah QLD
Share this page Provide feedback on this investigation
Last update 21 October 2014