Pilot Debrief

PIPER PA28 near Butler, KY — 2018-05-27

Final reportGAA18CA307
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Date
2018-05-27
Location
Butler, KY, USA
Aircraft
PIPER PA28
Registration
N95410
Category
Airplane
Highest injury
None
Fatalities
0
Phase of flight
Descent

Probable cause

The pilot’s improper fuel management, which resulted in fuel starvation.

NTSB narrative

The pilot reported that, while en route, the airplane's engine began to run roughly and lose power. He immediately turned toward the nearest airport and slowed the airplane to 100 knots. He added that he pushed the mixture to full rich, which caused a short burst of power that lasted just a few seconds. He then pumped the throttle and applied carburetor heat but then realized he did not have enough altitude to make the airport and began to look for an alternate landing site. The pilot further added that, after locating a ridgetop field, he slowed the airplane to 75 knots and pulled one notch of flaps and trimmed for landing. As he lined the airplane up with the field, he pulled full flaps about 300 ft above the ground. The touchdown was smooth, and the airplane continued the landing roll in 3-ft-tall wheat. Subsequently, the right wing struck an industrial irrigation nozzle, and the right wing separated from the fuselage. The airplane sustained substantial damage to the right wing and stabilator. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot added that, during the engine failure, he did not attempt to change the fuel tank from the empty right wing fuel tank and recommended to make the fuel selector check the first part of the restart procedure. The Federal Aviation Administration inspector reported that, while on scene, he was able to run the engine. He added that the left tank was about 1/2 full of fuel. He switched the fuel selector to the left tank and started the engine normally. The oil pressure was fine; the fuel pressure was normal on both the electric pump and engine-driven pump; and the magnetos checked fine.

Analysis

Primary failure mode
Fuel management
First missed decision gate
Pilot did not switch fuel tanks from the empty right wing tank during engine failure.

NTSB coding

Evidence available

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

Docket documents4

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