Pilot Debrief

PIPER PA-12 near Columbia, MO — 2009-09-22

Final reportCEN09LA597
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Date
2009-09-22
Location
Columbia, MO, USA
Aircraft
PIPER PA-12
Registration
N3234M
Category
Airplane
Highest injury
Fatal
Fatalities
1
Phase of flight
Climb

Probable cause

The pilot's continued visual flight into instrument meteorological conditions, which included low ceilings and fog, and his failure to maintain control of the airplane. Contributing to the accident was the partial loss of engine power as a result of water contamination of the fuel.

Contributing factors

Contributing to the accident was the partial loss of engine power as a result of water contamination of the fuel.

NTSB narrative

Due to adverse weather conditions, the pilot landed at a grass airstrip en route to his destination. The airport manager stated that a front was approaching the airport and that it rained all night. According to the airport manager, the pilot returned to the airport the next morning, started the airplane, and taxied to the fuel pump. The right fuel cap was missing. He drained the fuel sump repeatedly because he found water in the right tank. The airport manager gave the pilot a fuel cap for the right tank so that he could depart. Witnesses reported seeing the airplane flying 50–60 feet above the ground with the engine sputtering and cutting in and out prior to the accident. Airplane impact damage was consistent with a steep nose-down attitude with about 80 degrees of left roll. Witnesses reported heavy cloud cover and limited visibility due to light-to-moderate fog. Observed weather near the accident site was 1/4 mile visibility in fog with an indefinite ceiling at 100 feet. The Weather Depiction Chart depicted an area of instrument-flight-rule (IFR) conditions along and behind the cold front. The accident site was located in an area of IFR conditions, with the departure and planned destination airports under visual flight rules (VFR) conditions. The pilot was not instrument rated, and the airplane was not equipped for IFR flight. The inspection of the engine and airframe revealed no preimpact anomalies. The propeller blades were bent aft from impact forces.

Analysis

Primary failure mode
VFR into IMC
First missed decision gate
Pilot did not obtain a preflight weather briefing before departure.

NTSB coding

Evidence available

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

Docket documents22

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