NTSB CAROL · Event
Event CEN13LA525
Aircraft involved
Probable cause & findings
The pilot's failure to adequately clear carburetor icing, resulting in a loss of engine power on final approach following a descent at idle power.
Factual narrative
**This report was modified on 1/30/2014. Please see the public docket for this accident to view the original report.** On September 1, 2013, about 1100 mountain daylight time, a Cessna 182 airplane, N6460A, was substantially damaged when the pilot ditched the airplane into a lake following a loss of engine power on approach to the Boulder Municipal Airport (BDU), Boulder, Colorado. The pilot sustained minor injuries. The airplane was registered to and operated by N6460A LLC under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from BDU about 1035. The pilot reported that he had flown a group of skydivers to altitude for an intentional parachute jump about 3 miles north of the airport and was returning for landing at the time of the accident. The airplane was on final approach to runway 8 (4,100 feet by 75 feet, asphalt) when the engine lost power. His attempts to restore engine power were unsuccessful and he subsequently ditched into Hayden Lake short of the runway. He reported a clear sky with a light and variable wind. A postaccident engine examination conducted by a National Transportation Safety Board investigator did not reveal any anomalies consistent with a preimpact failure or malfunction. Approximately 11 gallons of fuel were recovered from the airplane after the accident. The Pilot's Operating Handbook for the accident airplane noted that up to 5 gallons of fuel is unusable in all flight conditions, with 2 gallons of fuel being unusable in level flight. Weather conditions recorded at the Rocky Mountain Metropolitan Airport (BJC), located about 9 miles southeast of BDU, at 1047, included an ambient temperature and dew point of 21 degrees Celsius and 11 degrees Celsius, respectively. According to a Federal Aviation Administration (FAA) inspector, the pilot had reported using carburetor heat during the descent after the skydivers left the airplane; however, the pilot did not periodically apply engine power (clear the engine) during the descent. Information provided by the FAA regarding carburetor icing noted a possibility of serious icing at glide power under those conditions. According to FAA Advisory Circular 20-113, Pilot Precautions and Procedures to be Taken in Preventing Aircraft Reciprocating Engine Induction System and Fuel System Icing Problems, "Heat should be applied for a short time to warm the induction system before beginning a prolonged descent with the engine throttled and left on during the descent. Power lever advancement should be performed periodically during descent to assure that power recovery can be achieved." The pilot reported that he had flown a group of skydivers to altitude for an intentional parachute jump about 3 miles north of the airport and was returning for landing at the time of the accident. The airplane was on final approach when the engine lost power. The pilot's attempts to restore engine power were unsuccessful, and he ditched the airplane into a lake short of the runway. The pilot reported using carburetor heat during the descent; however, the pilot did not periodically apply engine power (clear the engine) during the descent. According to FAA Advisory Circular 20-113, Pilot Precautions and Procedures to be Taken in Preventing Aircraft Reciprocating Engine Induction System and Fuel System Icing Problems, "Heat should be applied for a short time to warm the induction system before beginning a prolonged descent with the engine throttled and left on during the descent. Power lever advancement should be performed periodically during descent to assure that power recovery can be achieved." A postaccident engine examination did not reveal any anomalies consistent with a preimpact failure or malfunction. Local weather conditions were conducive to the formation of carburetor icing. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-Conducive to carburetor icing-Effect on equipment - C
- C Aircraft-Aircraft power plant-Engine (reciprocating)-(general)-Inoperative - C
- C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2013_CEN13LA525.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 ↗