NTSB CAROL · Event
Event CEN21LA231
Registry · N5578G
FAA Aircraft Registry record.
Make / Model
CESSNA 150J
Year of manufacture
1969 · 52 years old at event
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19691020
ADS-B equipped
Yes — Mode-S A71CE3
Registrant of record
GILBREATH JOHN W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s improper fuel planning which led to fuel exhaustion, and a total loss of engine power.
Factual narrative
On April 28, 2021, about 1230 central daylight time, a Cessna 150J, N5578G, was substantially damaged when it was involved in an accident near Madison, Arkansas. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, while the airplane was in cruise flight, the engine power reduced to idle. The pilot noted that the engine was still running, but he was unable increase power above idle. He stated that the engine acted as if the throttle control was disconnected. The pilot subsequently made a forced landing to a field. During the forced landing, the airplane’s nose landing gear sunk in the soft ground, and the airplane nosed over. The airplane sustained substantial damage to the vertical stabilizer and the right wing. Examination of the accident site revealed no sheen of fuel on the water in the field and a “light” smell of fuel. The recovery crew that moved the airplane from the field reported that “only ounces” of fuel remained in the wing fuel tanks. After the airplane was moved, a subsequent examination was performed, which found no fuel in the gascolator. Also, the carburetor had broken loose from its mount, but the throttle cable remained attached to the carburetor, and movement of the throttle control caused movement of the carburetor butterfly. A weather observation for a nearby airport indicated that the temperature and dew point were 25°C and 20°C, respectively. According to the carburetor icing probability chart in the Federal Aviation Administration’s Special Airworthiness Information Bulletin CE-09-35, Carburetor Icing Prevention, these temperatures were in the range for serious icing at glide power. The pilot reported that, while the airplane was in cruise flight, the engine power reduced to idle. The pilot noted that the engine was still running but that he was unable to increase power above idle. He stated that the engine acted as if the throttle control was disconnected. The pilot made a forced landing to a field. During the forced landing, the airplane’s nose landing gear sunk in the soft ground, and the airplane nosed over. Examination of the airplane after the accident revealed no usable fuel remaining in the wing fuel tanks, no fuel in the gascolator, and no evidence of a fuel spill at the accident site. The throttle control connection was checked; although the carburetor had broken loose from its mount due to impact, evidence indicated that the throttle control was functioning. The temperature and dew point at the time of the accident were conducive for carburetor icing at glide power. However, a power loss during cruise flight and power that rapidly reduces to idle are not consistent with a loss of power due to carburetor icing. Given the available evidence for this investigation, the pilot failed to adequately plan the fuel for the flight which resulted in the airplane’s fuel supply to be exhausted, resulting in a total 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 level
- — Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2021_CEN21LA231.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 (icing, fuel exhaustion). 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 2019 · Contractor Report (CR)
A study of carburetor/induction system icing in general aviation accidents
An assessment of the frequency and severity of carburetor/induction icing in general-aviation accidents was performed. The available literature and accident data from the National Transportation Safet…
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
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