NTSB CAROL · Event
Event FTW92LA097
Registry · N5529S
FAA Aircraft Registry record.
Make / Model
CESSNA R182
Year of manufacture
1980 · 12 years old at event
Engine
LYCOMING 0-540 SERIES (250 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19800612
ADS-B equipped
Yes — Mode-S A70A7D
Registrant of record
P & M AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE COMPLETE LOSS OF ENGINE POWER DUE TO CARBURETOR ICING, AND THE PILOT'S DELAYED APPLICATION OF CARBURETOR HEAT. FACTORS WERE THE WEATHER CONDITIONS WHICH WERE HIGHLY CONDUCIVE TO CARBURETOR ICING, AND THE UNSUITABLE TERRAIN AT THE PILOT'S DISPOSAL TO EXECUTE A SUCCESSFUL FORCED LANDING.
Factual narrative
THE PILOT WAS ESTABLISHED ON FINAL APPROACH TO THE DESTINATION AIRPORT WHEN THE ENGINE STARTED TO RUN ROUGH. DESPITE EFFORTS BY THE PILOT TO REMEDY THE SITUATION, INCLUDING APPLICATION OF CARBURETOR HEAT, THE ENGINE LOST POWER. A FORCED LANDING WAS MADE IN A MUDDY FIELD. DURING ROLLOUT THE NOSE WHEEL DUG INTO THE SOFT GROUND, PARTIALLY COLLAPSING THE NOSE WHEEL ASSEMBLY AND CAUSING THE AIRPLANE TO NOSE OVER ON ITS BACK. WEATHER CONDITIONS AT THE TIME OF THE ACCIDENT WERE HIGHLY CONDUCIVE TO CARBURETOR ICING. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_FTW92LA097.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 ↗