NTSB CAROL · Event
Event CEN22LA237
Registry · N8283V
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-161
Year of manufacture
1980 · 42 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19801010
ADS-B equipped
Yes — Mode-S AB5168
Registrant of record
MILOUD CHADD K
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot’s inadequate fuel management that resulted in a loss of engine power due to fuel starvation.
Factual narrative
On June 7, 2022, about 1415 central daylight time, a Piper PA-28-161 airplane, N8283V, was substantially damaged when it was involved in an accident near Fort Worth, Texas. The student pilot was not injured. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as an instructional flight. The solo student pilot returned from a cross-country flight and planned on practicing touch-and-go landings. After the first touch-and-go landing to runway 17, when the airplane was about 100 ft above ground level, the airplane’s engine stopped producing power. The student pilot performed a forced landing straight ahead. During the landing, the airplane’s left wing contacted a tree and separated resulting in substantial damage. A Federal Aviation Administration (FAA) inspector responded to the accident site and examined the airplane. He found that the fuel selector was selected to the left fuel tank, which was about half full of fuel. The right fuel tank was empty. The student pilot reported to the FAA inspector that the fuel selector was on the right tank when the engine stopped producing power. The student pilot stated the selector was moved to the left tank position when the airplane was being secured after the accident. The student pilot was practicing a touch-and-go landing following a cross-country flight when the accident occurred. During the takeoff portion of the touch and go, at an altitude of 100 ft above the runway, the engine stopped producing power. The student pilot performed a forced landing and the left wing collided with a tree and separated which resulted in substantial damage. A postaccident examination of the airplane found the right fuel tank was empty and the left fuel tank was about ½ full of fuel. The student pilot reported the right fuel tank was selected when the engine lost power. It is likely that the engine lost power when it was starved of fuel. 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-Use of equip/info-Use of equip/system-Student/instructed pilot
Verbatim from NTSB's published report. Source file
NTSB_2022_CEN22LA237.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 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 · 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…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗