NTSB CAROL · Event
Event CHI01LA023
Registry · N94176
FAA Aircraft Registry record.
Make / Model
ENGINEERING & RESEARCH ERCOUPE 415-E
Engine
CONT MOTOR C85 SERIES (85 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19721013
ADS-B equipped
Yes — Mode-S AD144B
Registrant of record
WOOD MICHAEL E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the carburetor ice and after takeoff, the unsuitable terrain the pilot encountered during the forced landing. Factors were the carburetor icing conditions and the plowed field condition.
Factual narrative
On October 23, 2000, about 1600 central daylight time, an Ercoupe 415-E, N94176, piloted by a commercial pilot, encountered an in-flight loss of engine power and sustained substantial damage on contact with terrain during a forced landing in a plowed field near Minier, Illinois. The personal flight was operating under 14 CFR Part 91. Visual meteorological conditions prevailed at the time of the accident. No flight plan was on file. The pilot was uninjured. The flight was on initial climbout from the Illinois Valley Parachute Club Airport, near Minier, Illinois and was destined for Capital Airport, near Springfield, Illinois. The pilot stated, "The takeoff went as normal, power from engine was 2350 RPM at full throttle[.] Fuel pressure guage showed 4.5 "(p.s.i.). At 70 M.P.H. climb speed, the engine lost power at approx. 300 ft. A.G.L.[.] Applied carb heat, pumped the throttle, ck. elect. pump on O.K. - no power - turned 45 [degrees] landed. In field. (Plowed fld.)" A Federal Aviation Administration inspector performed an on-scene examination of the airplane. No anomalies were listed in the inspector's statement. All the spark plugs were found covered with "black soot looking deposits." At 1550, the Central Illinois Regional Airport at Bloomington-Normal Airport, near Bloomington/Normal, Illinois, weather observation was: Wind 200 degrees at 5 knots; visibility 7 statute miles; sky condition broken 9,000 feet overcast 18,000 feet; temperature 24 degrees C; dew point 16 degrees C; altimeter 30.38 inches of mercury. A copy of a Transport Canada Carburetor Icing chart was reviewed. The temperature and dew point were plotted on the chart and their intersection falls in the moderate icing - cruise power or serious icing - descent power area of the chart. See appended icing chart. The airplane encountered an in-flight loss of engine power and sustained substantial damage on contact with terrain during a forced landing in a plowed field. The pilot was uninjured. The pilot stated, "The takeoff went normal, power from engine was 2350 RPM at full throttle fuel pressure guage showed 4.5 "(p.s.i.). At 70 M.P.H. climb speed, the engine lost power at approx. 300 ft. A.G.L. applied carb heat, pumped the throttle, ck. elect. pump on O.K. - no power - turned 45 [degrees] landed. In field. (Plowed fld.)" An on-scene examination of the airplane revealed no anomalies. All the spark plugs were found covered with "black soot looking deposits." The temperature was 24 degrees C and the dew point was 16 degrees C. A copy of a Transport Canada Carburetor Icing chart was reviewed. The temperature and dew point were plotted on the chart and their intersection falls in the moderate icing - cruise power or serious icing - descent power area of the chart. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_CHI01LA023.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 ↗