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During the take-off run the pilot sensed a loss of power being transmitted to the propeller. He assessed that he could not stop in the strip length remaining and reduced the throttle setting in the hope that the reduction drive would transmit the reduced power to the propeller. The aircraft cleared the fence at the end of the strip, but the pilot was forced to turn through about 90 degrees to avoid a power line and to line up with the contours of the ploughed field he had selected for a forced landing. During this turn the airspeed reduced to the point where a high sink rate developed, and the pilot had insufficient height or power to effect a recovery before the aircraft mushed into the ground. On impact, the left mainwheel was torn off and the aircraft overturned some five metres beyond the initial touchdown point. Specialist investigation showed that disc springs had been incorrectly replaced during a modification to the reduction gearbox. This allowed the dog gear to ride up and out of the dog hub, under the reduced stiffness of the axial spring assembly, and reduce the transmission of power to the propeller. Investigation also revealed that there was some ambiguity in the assembly instructions for the gearbox modification.

Download Final Report
[ Download PDF: 23KB]
General details
Date: 28 March 1988 Investigation status: Completed 
Time: 700  
Location:Lindsay Point (28 km ENE of Renmark) Investigation type: Occurrence Investigation 
State: Victoria Occurrence type: Propeller/rotor malfunction 
Release date: 21 October 1988 Occurrence class: Technical 
Report status: Final Occurrence category: Accident 
 Highest injury level: None 
Aircraft details
Aircraft manufacturer: TL Ultralight 
Type of operation: Private 
Damage to aircraft: Substantial 
Departure point:Lindsay Point VIC
Destination:Lindsay Point VIC
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Last update 15 March 2016