Pilot Debrief

PIPER PA28 near Dwight, IL — 2019-04-19

Final reportCEN19LA126
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Date
2019-04-19
Location
Dwight, IL, USA
Airport
DTG
Aircraft
PIPER PA28
Registration
N838JH
Category
Airplane
Highest injury
None
Fatalities
0
Phase of flight
Cruise

Probable cause

A partial loss of engine power due to a restriction in fuel flow for undetermined reasons.

NTSB narrative

The pilot was in cruise flight in the single-engine airplane when the engine started to run rough. He applied carburetor heat, but the engine continued to run rough. He noticed that the fuel pressure gauge indicated 0, so he turned on the electric fuel boost pump, which did not restore power. He then switched fuel tanks, which momentarily restored engine power. The pilot decided to divert to a nearby airport and continued to switch between fuel tanks to obtain short bursts of engine power. During landing, the airplane departed the runway surface and the nose landing gear collapsed. Examination of the fuel system found available fuel in the tanks and only a small amount of debris in the gascolator. Both the engine-driven and electric fuel boost pumps were removed from the airplane. Hand testing of the engine-driven pump found suction and pressure at the inlet and outlet ports. Testing of the electric boost pump revealed that liquid would not flow when activated. Despite the failure of the electric boost pump, it was not indicated for use in cruise flight, and its failure should not have resulted in a loss of fuel flow. It is possible that an unidentified fuel restriction prevented fuel from getting to the engine-driven fuel pump; however, the reason for or source of the fuel restriction could not be determined during postaccident examination.

Analysis

Primary failure mode
Fuel management
First missed decision gate
Pilot could have landed earlier when first experiencing engine roughness.

NTSB coding

Evidence available

  • 1 docket document
View NTSB final reportView NTSB docket

Docket documents1

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