NTSB CAROL · Event
Event DEN03IA054
Registry · N214SW
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-14
Year of manufacture
2016
Engine
LYCOMING IO-390 SER (210 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20160413
ADS-B equipped
Yes — Mode-S A1CA03
Registrant of record
POWELL MARK
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the captain's failure to maintain directional control during takeoff. Factors contributing to the accident were the crew's diverted attention, the snow and slush-covered runway, the fog, and the runway marker.
Factual narrative
On March 16, 2003, at 2245 mountain standard time, an Embraer EMB-120ER, N214SW, operating as SkyWest Airlines Flight 3622, and piloted by an airline transport pilot, sustained minor damage during takeoff roll, when the airplane departed the left side of runway 20 (7,802 feet by 150 feet, slush/snow-covered, asphalt) at the Cedar City Municipal Airport (CDC), Cedar City, Utah, and struck a runway remaining marker before coming to a stop. Night instrument meteorological conditions prevailed at the time of the incident. The scheduled, domestic, passenger service flight was being conducted on an instrument flight rules flight plan from CDC to St. George, Utah, under the provisions of Title 14 CFR Part 121. The captain, first officer, flight attendant, and 12 passengers reported no injuries. The flight was originating at the time of the incident. The captain reported they were due to takeoff at 2136. The airplane was delayed approximately 17-18 minutes at the end of the runway awaiting clearance. During that time, approximately 1/4-inch of snow had accumulated on the airplane. The captain reported they went back to the ramp area to be de-iced. While being de-iced, the captain reported they coordinated with air traffic control to expedite their departure. The captain reported they taxied from the ramp to the runway and began the takeoff roll. The captain said that everything was fine initially. When they passed the 7,000 foot remaining marker, the airplane began tracking left. The captain said he tried to correct the situation with rudder and differential power, but the airplane continued to track left. The captain said, "I lost control of the situation when the left mains got into the soft earth at the edge of the runway." The first officer reported that just after they had advanced the power levels forward, the Ice Condition light illuminated. The first officer notified the captain and noticed that the airplane was pulling to the left. The first officer said the captain was attempting to correct the condition when the airplane pulled hard left. The airplane was straddling the runway lights. The first officer said the captain then aborted the takeoff. The first officer said that with braking, they slid off the runway and slowly spun to the left leaving the airplane facing east when it stopped. The airport manager reported that at the time of the incident, the runway was covered with 1 to 1-1/2 inches of snow. He said the bottom 1/4 inch of the snow was slush. The airport manager said he verified the runway lights were on and bright and the signs were lit. The airport manager said he examined the tire tracks in the snow and reported the airplane began its takeoff roll to the left of the runway centerline. The airport manager reported the tire tracks proceeded further left of centerline as they proceeded down the runway until they were off the left side of the runway. The airplane came to a stop just off of the left side of runway 20, approximately 2,400 feet down. An examination of the airplane showed that both propellers' blades were torsionally bent and curled at the tips. The rotating beacon on the bottom of the airplane's fuselage was broken aft. Fuselage skin in the vicinity of the beacon was torn and wrinkled. There were also several punctures in the lower fuselage skin. An examination of the airplane's systems revealed no anomalies. The reported weather at CDC at the time of the incident was ceilings 400 feet broken, 1,100 feet overcast, visibility 1/2 mile, snow and fog, temperature and dew point 32 degrees Fahrenheit, and an altimeter setting of 29.59 inches of Mercury. The captain reported they coordinated with ATC to expedite their takeoff due to the poor weather conditions. Following de-icing, the crew taxied the airplane from the ramp to the runway and began their takeoff roll. The captain said that everything was fine initially. When the airplane passed the 7,000 foot remaining marker, it began tracking left. The captain said he tried to correct the situation with rudder and differential power, but the airplane continued to track left. The captain said, "I lost control of the situation when the left mains got into the soft earth at the edge of the runway." The first officer reported that just after they had advanced the power levels forward, the Ice Condition light illuminated. The first officer notified the captain. The first officer stated that the airplane was pulling to the left. The first officer said the captain was attempting to correct the condition when the airplane pulled hard left. The airplane was straddling the runway lights. The first officer said the captain aborted the takeoff. The first officer said that with braking, they slid off the runway and slowly spun to the left leaving the airplane facing east when it stopped. The airport manager reported that at the time of the incident, the runway was covered with 1 to 1-1/2 inches of snow and slush. An examination of the airplane's tire tracks in the snow showed the airplane began its takeoff roll to the left of the runway centerline. The tracks proceeded further left of centerline as they proceeded down the runway until they were off the left side of the runway. An examination of the airplane revealed no anomalies. The reported weather at the time of the incident was ceilings 400 feet broken, 1,100 feet overcast, visibility 1/2 mile, snow and fog, temperature and dew point 32 degrees F, and an altimeter setting of 29.59 inches of Mercury. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_DEN03IA054.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 ↗