Aviation safety investigations & reports

Conaero LA4-200, VH-FOB, Cockburn Sound (21km Southwest of Jandakot) WA, 29 May 1988

Investigation number:
198800123
Status: Completed
Investigation completed

Summary

Download Final Report
[Download  PDF: 24KB]
 

The pilot had flown the aircraft to Cockburn Sound to practice circuits. However, after the first landing he found the water conditions too rough to complete a takeoff. The pilot waited for a period in the hope that conditions would improve. Three quarters of an hour later he taxied along Cockburn Sound looking for an area that was suitable for takeoff, but this search was unsuccessful. After beaching the aircraft a second time the pilot observed that the aircraft was taking water. When the pilot attempted to drain the excess water from the bilges he found that the rear bilge pump was unserviceable, and the water had to be drained manually by removing two bungs. The bungs were replaced when the water flow reduced to a trickle after five to ten minutes. The sea state abated after four hours and the pilot decided to carry out a high-speed taxy run during which, if he assessed the conditions were suitable, he could convert the run to a takeoff. The pilot was able to get the aircraft up on to the hull step, however, before he could continue with the takeoff the aircraft suddenly pitched nose-up and then down before nosing over inverted approximately 50 metres from the shore line. Neither occupant was wearing a life jacket although they were carried in the aircraft. Both occupants received injuries which may have required the jackets for survival had assistance not been given from the shore. A screw was found to be missing from a normally watertight panel on the rear fuselage. The screw had been missing since the aircraft was last painted. Tests indicated that water was able to leak into the aircraft via the missing screw hole. Water in the rear fuselage would normally be pumped out by the rear bilge pump, however, it was unserviceable. The pump's impeller had become detached from the drive shaft sometime prior to the accident flight. Tests on the manual draining system used by the pilot indicated that a minimum of 31 litres of water remained in the aft fuselage after draining was apparently complete, when the flow of water had slowed to a trickle. Although the sea state appeared to improve there was still a significant swell running at the time of the accident. The pilot attempted his high- speed run in the direction of the swell instead of parallel to it. It is probable that the combination of an aft centre of gravity, movement of weight associated with the water in the fuselage and the uplift provided by the swell caused the loss of control.

Download Final Report
[Download  PDF: 24KB]
 
 
 
General details
Date: 29 May 1988   Investigation status: Completed  
Time: 1619    
Location: Cockburn Sound (21km Southwest of Jandakot)    
State: Western Australia   Occurrence type: Loss of control  
Release date: 10 January 1989   Occurrence category: Accident  
Report status: Final   Highest injury level: Serious  

Aircraft details

Aircraft details
Aircraft manufacturer Lake A/C Div. Of Consolidated Aeronautics Inc.  
Aircraft model LA-4  
Aircraft registration VH-FOB  
Serial number 970  
Type of operation Private  
Damage to aircraft Destroyed  
Departure point Cockburn Sound WA  
Departure time 1619  
Destination Jandakot WA