Pilot Debrief

HUGHES HELICOPTERS INC 369E near The Dalles, OR — 2012-07-26

Final reportWPR12LA328
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Date
2012-07-26
Location
The Dalles, OR, USA
Airport
KDLS
Aircraft
HUGHES HELICOPTERS INC 369E
Registration
N427WC
Category
Helicopter
Highest injury
Serious
Fatalities
0
Phase of flight
Hover

Probable cause

The loss of engine power due to fuel starvation, which resulted from the fuel tank supply pickup becoming unported while the helicopter was pulling power lines.

NTSB narrative

The operator reported that the helicopter was in an 80-ft hover and had begun lifting and dragging the ends of winch lines used to pull power cables across sloping terrain when the engine lost power. The pilot jettisoned the external load as the helicopter began to descend rapidly. The helicopter's tail boom contacted the ground first and was then cut by the main rotor system, the skids separated from the fuselage, and the helicopter then came to rest on its right side. Several witnesses reported that the engine was still running on the ground after the impact. Postaccident examination and operational testing of the engine revealed no anomalies that would have precluded normal operation. During previous investigations of similar accidents, it was determined that the fuel tank supply pickup can become unported with a fuel load of less than 151 lbs when pitch-and-roll attitudes approach 20 degrees; the operator reported that about 117 lbs of fuel was recovered from the helicopter. It is likely that the fuel tank supply pickup unported while the helicopter was maneuvering, which led to fuel starvation and the subsequent loss of engine power.

Analysis

Primary failure mode
Engine power loss
First missed decision gate
Pilot could have aborted the operation before losing engine power.

NTSB coding

Evidence available

  • Photos
  • 9 docket documents
View NTSB final reportView NTSB docket

Docket documents9

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