Pilot Debrief

KINSLER ARTHUR PAUL KINSLER LANCAIR/MKII near Crivitz, WI — 2014-05-06

Final reportCEN14LA241
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Date
2014-05-06
Location
Crivitz, WI, USA
Aircraft
KINSLER ARTHUR PAUL KINSLER LANCAIR/MKII
Registration
N246AK
Category
Airplane
Highest injury
Serious
Fatalities
0
Phase of flight
Climb

Probable cause

The improper installation of the hose fuel fitting, which resulted in the fitting becoming disconnected and the subsequent loss of engine power due to fuel starvation.

NTSB narrative

The pilot reported that, about 10 to 15 minutes after takeoff in the single-engine airplane, he smelled fuel in the cockpit, and the airplane's fuel pressure gauge read 0. He activated the electric fuel boost pump, but the fuel pressure reading remained 0. At this point, the engine lost power, and the pilot subsequently executed a wheels-up forced landing to a field. Postaccident examination of the airplane revealed that the inlet hose to the mechanical fuel pump was not connected; the hose fitting and the fuel pump's mating fitting were not damaged. Based on the available evidence, it is likely that the hose fuel fitting was not properly installed, which allowed the fitting to vibrate loose during operation until it became disconnected and resulted in the loss of engine power due to fuel starvation. Because the hose fitting was found higher than the fuel tanks, fuel would not have leaked from the hose while the airplane was parked. Therefore, the pilot would not have been able to detect the discrepancy during preflight examination of the airplane.

Analysis

Primary failure mode
Engine power loss
First missed decision gate
Pilot could have checked fuel system before takeoff to ensure proper connections.

NTSB coding

Evidence available

  • 2 docket documents
View NTSB final reportView NTSB docket

Docket documents2

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