Pilot Debrief

PIPER PA32 near Bartow, FL — 2016-10-31

Final reportERA17LA034
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Date
2016-10-31
Location
Bartow, FL, USA
Airport
BOW
Aircraft
PIPER PA32
Registration
N3941X
Category
Airplane
Highest injury
None
Fatalities
0
Phase of flight
Approach

Probable cause

A total loss of engine power during approach for reasons that could not be determined because engine examinations did not reveal any evidence of mechanical malfunctions or failures that would have precluded normal operation.

NTSB narrative

While approaching the airport, the private pilot reduced engine power in preparation for landing. At that time, the airplane began to vibrate and shake. The engine then lost total power, while the propeller continued to windmill. He attempted to restart the engine using the emergency checklist procedures but was unsuccessful. He determined that he would not be able to reach the runway and maneuvered toward a nearby pasture for an emergency landing. During the landing rollout, the airplane struck a fence, damaging the left wheel hydraulic brake line, which caused a loss of brake pressure. When the pilot applied the brakes, he lost directional control, and the nose landing gear collapsed. Postaccident examination of the airplane revealed that the firewall was damaged and the fuselage skin aft of the firewall was wrinkled. An unmeasured amount of fuel was present in all four fuel tanks, and fuel was present at the fuel injector nozzles; thus, adequate fuel was onboard for the flight. Oil was present in the crankcase, and cylinder compression was attained on all cylinders when the propeller was rotated by hand. While rotating the engine, a grinding/crunching noise occurred once but was not repeatable. A subsequent partial teardown examination of the engine did not reveal any evidence of mechanical malfunctions or failures that would have precluded normal operation. Thus, the reason for the total loss of engine power could not be determined.

Analysis

Primary failure mode
Engine power loss
First missed decision gate
Pilot could have aborted the approach after initial engine power loss.

NTSB coding

Evidence available

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

Docket documents5

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