Pilot Debrief

Cessna T210L near Burleson, TX — 2020-05-07

Final reportCEN20LA172
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Date
2020-05-07
Location
Burleson, TX, USA
Airport
FWS
Aircraft
Cessna T210L
Registration
N2074S
Category
Airplane
Highest injury
Fatal
Fatalities
1
Phase of flight
Initial climb

Probable cause

The loss of engine power due to fuel starvation.

Contributing factors

Findings Environmental issues Tree(s) - Contributed to outcome Aircraft Fuel - Fluid management Personnel issues Use of available resources - Pilot

NTSB narrative

The pilot had just departed the runway for a second circuit in the traffic pattern. Shortly thereafter, he declared an emergency but did not indicate the nature of the emergency. A witness said he heard the "loud strong engine sound suddenly and drastically reduce to either power off or a low idle." He saw the airplane fly level for a few seconds then descend slowly toward the ground; the wings banked slightly one way, then the other. He stated that the airplane continued flying straight while descending, that the wings began to rock slightly, and that when the airplane was about 10 to 20 ft above the tree line, its “rate of descent accelerated into the trees." The airplane struck tree-covered terrain and impacted the ground about 1/2 mile south of the runway. A postcrash fire ensued and destroyed the airplane. Postaccident examination of the engine revealed no anomalies that would have precluded normal operations. The damage signatures on the propeller were consistent with little to no power at the time of impact. The examination revealed that the inboard portion of the right wing was partially consumed by the fire, but the remainder of the wing exhibited no fire damage. The right fuel tank area of the wing appeared undamaged, and the right fuel tank was empty. The left wing was consumed by fire, and given the extent of fire damage, the fuel tank likely contained fuel. The fuel selector valve appeared to be selected to the left tank but was about 5° counterclockwise past the left tank position and was not secure in the detent. The engine-driven fuel pump’s driveshaft was intact and there was no fuel in the fuel pump. Based on the available evidence, it is likely that the engine lost power due to fuel starvation. It is unknown if the pilot selected the left tank before takeoff or after the loss of engine power. With the fuel selector valve not placed in the detent for the left fuel tank, fuel would not be able to flow from the tank to the engine and the engine would have lost power.

Analysis

Primary failure mode
Fuel management
First missed decision gate
Pilot could have refueled before the second takeoff to ensure adequate fuel.

NTSB coding

Evidence available

  • 15 docket documents
View NTSB final reportView NTSB docket

Docket documents15

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