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J10/2/7227 A00-084 SOUTH AFRICAN CIVIL AVIATION AUTHORITY
ACCIDENT
REPORT
EXECUTIVE
SUMMARY
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Date of Accident
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04/08/2000 |
Time of Accident |
0920z |
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Aircraft Registration |
ZS-HKP |
Type of Aircraft |
Bell 206B |
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Pilot-in-command Licence Type
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Private
Pilot Licence |
Licence Valid
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Yes |
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Pilot-in-command Flying
Experience
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Total
Flying Hours |
Heli
74.1 hrs Aero 2050 hrs |
Total
Hours on Type |
Heli 14.4 hrs |
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Type of Operation |
Private
flight |
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Last point of departure |
Farm
in Witriver area |
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Next point of intended landing
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Mine
at Steelpoort |
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Location of the accident
site with reference to easily defined geographical points (plus GPS readings
if possible) |
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On
the farm Welgevonden in the Steelpoort district (S24°46.503' E030°17.667'). |
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Meteorological
Information |
Weather
was fine. |
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Number of people on board |
1
+ 1 |
No. of people injured
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Nil
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No. of people killed
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1 + 1 |
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Synopsis
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The
pilot bought the helicopter a few weeks before the accident and completed his
conversion training 4 days after he accepted the helicopter. He flew the helicopter back to Lanseria
Airport in order that the turbine module of the engine could be
exchanged. On the morning of the
accident, the pilot/owner of the helicopter flew from his farm in the
Witriver area to a mine in the Steelpoort area. A witness stated the rotor blades were rotating at a lower rate
than he was used to when helicopters fly over the farm. He indicated that the
helicopters flew lower than what he was used to and it appeared to him that
the main rotor was losing rotational speed and nearly became stationary. All this time the helicopter was losing
height and at approximately 20 m above the ground the helicopter fell almost
vertically to the ground. During the investigation the compressor to turbine coupler in the engine was found fractured and different opinions were expressed as to the reason for the failure of the coupler and the engine. |
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Probable Cause |
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The engine failed during flight and the pilot
was unable to execute a successful autorotation. The cause of the engine failure could not be conclusively
established. |
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