NTSB CAROL · Event
Event ANC23LA006
Registry · N23CF
FAA Aircraft Registry record.
Make / Model
CESSNA 207
Year of manufacture
1974 · 48 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19741219
ADS-B equipped
Yes — Mode-S A2065F
Registrant of record
YR-AIRCRAFT LEASING LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The total loss of engine power during cruise flight due to fuel starvation and the pilot’s mismanagement of the available fuel.
Factual narrative
On November 20, 2022, about 1140 Alaska daylight time, a Cessna 207 airplane, N23CF, was substantially damaged when it was involved in an accident near Bethel, Alaska. The commercial pilot and six passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 135 passenger flight. The flight departed from the Goodnews Bay Airport (GNU) at 1035, on a scheduled flight to the Bethel Airport (BET). While in cruise flight at 1,000 ft above ground level, about 8 minutes from BET, the engine experienced a partial loss of power. The pilot performed the emergency procedures but was unable to regain engine power. The pilot performed a forced landing to an area of ice-covered frozen tundra about 10 miles southeast of the airport. After landing the pilot contacted the operator’s dispatch for rescue. Examination of the photographs taken at the accident site revealed substantial damage to the right wing and fuselage. Examination of the airplane before recovery revealed the left fuel tank was full with about 40 gallons of fuel and the right fuel tank was empty. When power was applied to the airplane the fuel indicating system displayed the left fuel tank was almost full and the right fuel tank was empty. The airplane was recovered to the Bethel Airport for an engine examination. During the examination, no fuel was found in the fuel lines from the fuel selector in the cockpit to the engine. The damaged propeller was removed, and a serviceable propeller was installed. The engine fuel boost pump was used, and the engine started and ran normally. Visual inspection of the engine found no abnormalities. The pilot later stated he believed the engine had an engine oil pump issue and was concerned with using the fuel boost pump, fearing he was adding fuel to a possible fire. The pilot had little time to troubleshoot the engine problem and his main concern was finding a safe place to land. He said at about 75 to 100 ft above the ground, he switched the fuel selector to the left tank but did not turn on the fuel boost pump. The Cessna 207 fuel selector can only operate in the left or right fuel tank position. It is the operator’s procedure to change the selected fuel tank at the midpoint of the flight. While in cruise flight, the engine experienced a loss of power at 1,000 ft above ground level. The pilot performed the emergency checklist but was unable to restore engine power. He performed a forced landing to an area of ice-covered frozen tundra. Postaccident examination of the engine and fuel system revealed that the left fuel tank was full, and the right fuel tank was empty. No fuel was present in the fuel lines from the cockpit fuel selector to the engine. During the engine examination, the engine started and ran normally. Other than the absence of fuel, no anomalies were noted with the engine that would have precluded normal operation. The airplane’s fuel selector can only operate in the left or right fuel tank position. The operator’s procedure is to change the selected fuel tank at the midpoint of the flight; however, the pilot indicated after the engine examination that he likely forgot to switch fuel tanks. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Personnel issues-Task performance-Use of equip/info-Use of policy/procedure-Pilot
- — Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid level
- — Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2022_ANC23LA006.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall, fuel starvation). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗