A preliminary report by the ATSB into the four-fatality accident
near Condobolin on 2 December indicates that there was no distress
signal from the aircraft before it broke up in the vicinity of
thunderstorms.
The Australian Transport Safety Bureau's Preliminary Aviation
Safety Investigation Report into the Piper Chieftain aircraft
accident near Condobolin, NSW also found that structural failure
spread wreckage along a 4 km path.
An active frontal weather system, accompanied by a line of
frequent thunderstorms, was passing through the Condobolin area at
the time of the accident. There was no distress signal from the
aircraft, which had been cruising at 10,000 ft and was about 54 km
left of the planned track. The pilot had advised air traffic
control that he was diverting left due to weather.
The aircraft was en route from Archerfield to Swan Hill on 2
December 2005. On board were two pilots and two passengers. The
forecast weather was amended after the time of the aircraft's
departure from Archerfield to include reference to a line of
frequent thunderstorms slowly moving east within 111 km of a line
from Cobar to Wagga. That line crossed the intended track of the
aircraft. It has not yet been established if the pilot received the
amended weather information.
Examination of the wreckage revealed that both wings had failed
outboard of the engine nacelles and that the right engine had
separated from the aircraft. Sections of the rudder and horizontal
stabiliser had also separated. Some parts of the separated
structure were retrieved from the wreckage trail for further
examination. There was no evidence of hail or lightning strike
damage to the available pieces of wreckage. The available evidence
indicated that the engines were capable of normal operation prior
to the break-up.
The investigation is continuing and will include detailed
examination of the retrieved structural items, the weather
information and conditions, recorded air traffic control radar and
audio information, aircraft maintenance and pilot records.
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