NTSB CAROL · Event
Event CHI00LA046
Registry · N7339X
FAA Aircraft Registry record.
Make / Model
CESSNA 150B
Year of manufacture
1961 · 38 years old at event
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19611205
ADS-B equipped
Yes — Mode-S A9D9D9
Registrant of record
RENEWED INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilots failure to use carburetor heat during takeoff in weather conducive for serious carburetor ice. Factors were the weather that was conducive for carburetor icing and the presence of the truck that the aircraft impacted.
Factual narrative
On December 14, 1999, at 0910 central standard time, a Cessna 150B, N7339X, owned and piloted by a certified flight instructor (CFI), sustained substantial damage during a forced landing on a road, following an engine failure during climbout from the North Omaha Airport (3NO), Omaha, Nebraska. Visual meteorological conditions prevailed at the time of the accident. The local instructional flight was conducted under the provisions of 14 CFR Part 91 and was not on a flight plan. The CFI and dual student reported no injuries. The flight was originating at the time of the accident. In a written statement, the CFI stated, "shortly after departure, approximately 700 feet agl, 2,022 feet msl, the aircraft experienced a failed engine." The CFI stated that she executed a forced landing on a road and the aircraft contacted a semi-truck. A postaccident examination of the aircraft by the Federal Aviation Administration (FAA) revealed no preexisting anomalies with respect to the aircraft or aircraft systems. In a written report, the CFI reported no mechanical malfunction. The Eppley Airfield weather reporting station (OMA), Omaha, Nebraska, located 7 miles on a magnetic heading of 124 degrees from the accident site reported, at 0852, clear skies, winds from 090 degrees at 6 knots, an altimeter setting of 29.80 inches of mercury, a temperature of 32 degrees F., and a dewpoint of 28 degrees F. A carburetor icing probability chart developed by Transport Canada depicts regions of temperature and dewpoint that are conducive for the development of carburetor ice. FAA Advisory Circular AC 20-113 "Pilot Precautions and Procedures to be Taken in Preventing Aircraft Reciprocating Engine Induction System and Fuel System Icing Problems" states under Prevention Procedures, "When the relative humidity is above 50 percent and the temperature is below 70 degrees F., apply carburetor heat briefly immediately before takeoff, particularly with float type carburetors, to remove any ice which may have been accumulated during taxi and runup. The aircraft experienced an engine failure after departure. The certified flight instructor (CFI) executed a forced landing on a road where the aircraft wing contacted a semi-truck. A postaccident examination revealed no preexisting anomalies with respect to the aircraft or aircraft systems. The CFI reported no mechanical malfunction. A weather report stated a temperature of 32 degrees F., and a dewpoint of 28 degrees F. According to the carburetor icing chart by Transport Canada, the temperature and dewpoint at the time of the accident fall within the range of serious icing potential. FAA AC 20-113 states, 'When the relative humidity is above 50 percent and the temperature is below 70 degrees F., apply carburetor heat briefly immediately before takeoff, particularly with float type carburetors, to remove any ice which may have been accumulated during taxi and runup.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_CHI00LA046.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, engine failure). 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 ↗