Pilot Debrief

BELLANCA 17-30A near Washington, MO — 2023-12-30

Final reportCEN24LA077
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Date
2023-12-30
Location
Washington, MO, USA
Airport
FYG
Aircraft
BELLANCA 17-30A
Registration
N678MJ
Category
Airplane
Highest injury
Serious
Fatalities
0
Phase of flight
Initial climb

Probable cause

Fuel starvation and a total loss of engine power due to an obstructed fuel vapor return path. Contributing to the accident was the pilot’s inadvertent aerodynamic stall/spin, which likely increased the severity of the ground impact.

Contributing factors

Contributing to the accident was the pilot’s inadvertent aerodynamic stall/spin, which likely increased the severity of the ground impact.

NTSB narrative

The pilot reported that the engine start, run-up, and takeoff were without incident. However, shortly after takeoff, the engine completely lost power. In his efforts to avoid trees in the glide path, the airplane inadvertently entered an aerodynamic stall and spin. He was able to recover from the spin but unable to arrest the descent before impacting an open field. The airplane came to rest upright with damage to the fuselage, left wing, and empennage. The pilot reported that about three weeks before the accident a similar loss of engine power event occurred after takeoff. In that instance, he was able to land in the level grass area short of the runway without any damage to the airplane. A mechanic examined the airplane and noted that the diffuser was missing from the muffler. A postrecovery examination did not reveal any anomalies with the engine assembly. However, testing and disassembly of the fuel pump identified a piece of debris within the vapor ejector cavity. Further analysis determined that the material was a rubber fragment from a fuel line. The examination did not observe any indication that diffusers were installed in either the left or right mufflers. The fuel line fragment present in the pump likely traveled into a position in which it blocked the vapor return. This blockage then routed any fuel vapor into the fuel inlet line to the engine and resulted in an interruption of fuel flow due to vapor lock. The airplane maintenance records did not reveal a record of any recent work on the fuel pump or fuel lines. The investigation was unable to determine how the rubber fuel line fragment was introduced into the fuel system.

Analysis

Primary failure mode
Engine power loss
First missed decision gate
Pilot could have aborted the takeoff after the first power loss event.

NTSB coding

Evidence available

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

Docket documents10

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