Pilot Debrief

PIPER PA 23-160 near Port Clinton, OH — 2014-12-29

Final reportCEN15FA088
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Date
2014-12-29
Location
Port Clinton, OH, USA
Airport
KPCW
Aircraft
PIPER PA 23-160
Registration
N222CP
Category
Airplane
Highest injury
Fatal
Fatalities
1
Phase of flight
Takeoff roll

Probable cause

The pilot's loss of control following a loss of left engine power for reasons that could not be determined because an examination of the airframe and engine did not reveal any preimpact abnormalities.

NTSB narrative

The pilot was departing on a cross-country flight in the twin-engine airplane. A witness stated that before takeoff, the pilot spent about 20 minutes in the run-up area. As the airplane departed the runway, witnesses heard a "popping" noise come from the airplane. The airplane struggled to gain altitude, and one witness stated it appeared to have a problem with the left engine. The airplane turned left and descended. A review of a security camera video showed that the airplane turned left after takeoff, entered a rapid nose-down descent, and impacted terrain. A small amount of water was found in the left engine's carburetor; however, firefighter response efforts could not be eliminated as a potential source for the water. Based on the weather conditions at the time of the accident, the airplane was operating in an area associated with a risk of carburetor ice accumulation at glide and cruise power settings, but not at takeoff power settings. Witness reports and findings from the investigation are consistent with a loss of control following a loss of left engine power; however, the examination of the airframe and engines did not reveal evidence of any preimpact abnormalities.

Analysis

Primary failure mode
Engine power loss
First missed decision gate
Pilot could have aborted takeoff after hearing unusual engine sounds.

NTSB coding

Evidence available

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

Docket documents9

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