Pilot Debrief

PIPER PA 28-181 near Phoenix, AZ — 2014-02-04

Final reportWPR14FA111
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Date
2014-02-04
Location
Phoenix, AZ, USA
Airport
DVT
Aircraft
PIPER PA 28-181
Registration
N312PA
Category
Airplane
Highest injury
Serious
Fatalities
0
Phase of flight
Initial climb

Probable cause

The student pilot’s inadvertent positioning of the fuel selector in an intermediate position, which resulted in a loss of engine power due to fuel starvation.

NTSB narrative

The student and flight instructor were conducting touch-and-go landings. The student flew an approach that required slipping the airplane and maintaining a low engine power setting. During the climb after the touch-and-go landing, the airplane's engine lost power about 200 ft above ground level. The flight instructor stated that the engine's rpm was decreasing and he decided to turn toward the airport area. Subsequently, the flight instructor initiated a forced landing to a field near the airport. During the landing sequence, the airplane struck and breached the airport's perimeter fence and then nosed over; a postaccident fire ensued. The postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. During the examination of the airplane wreckage, the fuel selector was found in an intermediate position. Ground testing of a similar model airplane revealed that the engine could run several minutes with the fuel selector positioned in this intermediate position. The student and the instructor stated that the student switched the fuel selector about 9 miles from the airport per operator requirements to switch fuel tanks every 30 minutes. Because of the location of the fuel selector, the flight instructor could not visually confirm its position. It is likely that the student inadvertently positioned the airplane's fuel selector in an intermediate setting, which restricted the engine's fuel supply. Further, the engine's low power setting during the approach allowed the engine to run for several minutes on the fuel remaining in the return line and operate until shortly after the completion of the touch-and-go landing. Subsequently, during the climb, when the engine power was advanced, it is likely that the remaining fuel in the return line was exhausted and led to the engine power loss.

Analysis

Primary failure mode
Engine power loss
First missed decision gate
Fuel selector position not confirmed before takeoff, leading to power loss.

NTSB coding

Evidence available

  • 8 docket documents
View NTSB final reportView NTSB docket

Docket documents8

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