Pilot Debrief

CESSNA 210E near Port Orange, FL — 2012-01-25

Final reportERA12LA157
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Date
2012-01-25
Location
Port Orange, FL, USA
Airport
7FL6
Aircraft
CESSNA 210E
Registration
N7130U
Category
Airplane
Highest injury
Minor
Fatalities
0
Phase of flight
Maneuvering

Probable cause

The total loss of engine power for reasons that could not be conclusively determined during postaccident examination.

NTSB narrative

According to the pilot, it was the first flight after the engine installation. Prior to departure, he conducted a preflight engine run-up and all systems were normal. The airplane then departed and climbed to the traffic pattern altitude. While on the downwind leg of the traffic pattern, the engine failed. The pilot attempted to return to the airport but was unsuccessful and made a forced landing short of the runway in a heavily wooded area. An examination of the fuel did not reveal any contamination. While examination of the induction tubes revealed that the right side intake induction tube was not connected properly (the clamp was found tight but the rubber connection hose was not sealed), it may have become disconnected when the engine was dragged out from the accident site during recovery. Further, the engine manufacturer indicated that a loose intake induction tube would disrupt air flow but would not necessarily cause an engine to stop. Examination of the ignition system revealed that sections of the wiring were not sealed. Uninsulated or unsealed areas of the ignition system wiring could have caused grounding/shorting of the ignition system; however, the investigation was unable to conclusively determine the reason for the total loss of engine power.

Analysis

Primary failure mode
Engine power loss
First missed decision gate
Properly securing the intake induction tube before flight could have prevented engine failure.

NTSB coding

Evidence available

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

Docket documents10

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