NTSB CAROL · Event
Event CEN21LA341
Registry · N6162R
FAA Aircraft Registry record.
Make / Model
CESSNA T210F
Year of manufacture
1965 · 56 years old at event
Engine
CONT MOTOR GTSIO-520-C (340 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19651213
ADS-B equipped
Yes — Mode-S A807B6
Registrant of record
SMJD LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s fuel mismanagement that resulted in a complete loss of engine power during climb and subsequent impact with terrain during a forced landing.
Factual narrative
The pilot stated the engine began to run rough during climb after takeoff. To restore full engine power, the pilot selected the left and right fuel tanks numerous times. The engine subsequently experienced a complete loss of power, and the pilot performed a forced landing on a field about one mile south of the airport. The airplane sustained substantial damage that included damage to the horizontal stabilizer. Postaccident examination revealed that the airplane did not receive a recent annual inspection within the past 12 months, and there were several inspection panels within the airplane that were not installed. The right fuel tank was empty (except for unusable fuel), which resulted in fuel starvation and loss of engine power The pilot stated there was no mechanical malfunction/failure of the airplane. The pilot reported that during the climb after takeoff, the engine began to run rough. To restore full engine power, the pilot selected the left and right fuel tanks numerous times. The engine subsequently experienced a complete loss of power, and the pilot performed a forced landing to a field about one mile south of the airport during which the airplane impacted terrain. The airplane sustained substantial damage to the left horizontal stabilizer. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. A postaccident examination revealed the airplane’s left fuel tank contained useable fuel. The airplane’s right fuel was empty (except for unusable fuel), which resulted in fuel starvation and the loss of engine power. 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).
- — Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid management
- — Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot
- — Environmental issues-Physical environment-Terrain-Rough terrain-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2021_CEN21LA341.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 ↗