NTSB CAROL · Event
Event CEN22LA398
Aircraft involved
Probable cause & findings
The pilot’s failure to attain/maintain a proper glidepath that resulted in a hard landing and impact with the runway.
Factual narrative
On August 28, 2022, at 1345 eastern daylight time, a Cessna 172I, N46202, sustained substantial damage when it was involved in an accident near Olivet, Michigan. The student pilot was uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The student pilot was on a visual final for a low approach when he applied engine power to stabilize the descent. The engine did not respond, and the airplane continued to descend and landed hard land on the runway. The airplane nosed over and sustained substantial damage to both wings, the left wing strut, the fuselage, and the vertical stabilizer. The student pilot reported that he’d applied carburetor heat for about 10 seconds when he was about one mile from the runway. There was no engine roughness during the application. He then turned it off. Weather conditions were conducive for serious carburetor icing at glide power. A National Transportation Safety Board Pilot/Operator Aircraft Accident/Incident Report Form 6120.1 was not received from the student pilot. Postaccident examination of the airplane revealed that the left and right wing fuel tanks contained useable fuel. Examination of the airframe and engine revealed no mechanical anomalies that would have precluded normal operation. The student pilot was on a visual final for a low approach when he applied engine power to stabilize the descent. The engine did not respond, and the airplane continued to descend and landed hard on the runway. The airplane then nosed over and sustained substantial damage. Postaccident examination of the airplane revealed that the left and right wing fuel tanks contained useable fuel. Examination of the airframe and engine revealed no mechanical anomalies that would have precluded normal operation. The student pilot stated that the engine did not respond, but it is likely that the student pilot delayed the application of engine power and when he applied engine power, it exceeded the response capability of the airplane/engine that he perceived as delayed. The student pilot also reported that he’d applied carburetor heat for about 10 seconds when he was about one mile from the runway. There was no engine roughness during the application. He then turned it off. An accident report form was not received from the student pilot. Weather conditions were conducive for serious carburetor icing at glide 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-Aircraft oper/perf/capability-Performance/control parameters-Descent/approach/glide path-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2022_CEN22LA398.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). 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 ↗