CHI01LA023
2000-10-23 · MINIER, Illinois, United States · None · 1 aircraft · Status: Completed
Airport 81IL
Current FAA registration · N94176
- 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
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 ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (icing). All research papers
- arXiv 2026 · arXiv preprint Enabling Beyond-Visual-Line-of-Sight Drones Operation over Open RAN 5G Networks with Slicing
Among the foretold claims of the transition from 5G to 6G, Beyond-Visual-Line-of-Sight (BVLoS) drone operation has emerged as a prominent Internet-of-Robots enabler.
- 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…
- 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…
- 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…
- 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…