NTSB CAROL · Event
Event ANC12LA096
Registry · N2005E
FAA Aircraft Registry record.
Make / Model
TAYLORCRAFT AVIATION CORP. F21
Year of manufacture
1981 · 31 years old at event
Engine
LYCOMING 0-235 SERIES (115 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19810529
ADS-B equipped
Yes — Mode-S A1950F
Registrant of record
SHAW BRIAN W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain control of the airplane after a loss of engine power during takeoff due to carburetor ice.
Factual narrative
On September 2, 2012, about 1600 Alaska daylight time, a float-equipped Taylorcraft F21 airplane, N2005E, sustained substantial damage when it impacted the water during takeoff at Willow Lake Seaplane Base, Willow, Alaska. The airplane was being operated by the pilot as a visual flight rules (VFR) personal cross-country flight, under the provisions of 14 Code of Federal Regulations, Part 91, when the accident occurred. Visual meteorological conditions prevailed, and the solo pilot received serious injuries. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on September 3, the pilot said he had landed at the lake due to turbulence along his route of flight. After waiting about 30 minutes, he decided to depart. During takeoff, the airplane became airborne, but he did not think he would clear the trees at the end of the lake. He started a right turn to stay over the water, but as the turn steepened the airplane stalled, and impacted the lake. He said he did not know if the airplane's engine was producing full power. The right wing of the airplane was severed. In a written statement to the NTSB dated September 14, the pilot said after takeoff the engine began missing. He also indicated that the outside temperature was about 55 degrees F, and that it was raining. He further wrote that "maybe a more lengthy run-up to rule out carburetor ice" would have been appropriate. In an email to the NTSB IIC dated April 10, 2013, the pilot wrote that eventually the airplane had been salvaged from the lake, and sold for parts. He reported that the more he thought about the circumstances, the more he believed that the loss of power was the result of carburetor ice. The closest weather reporting facility was the Palmer Airport, about 10 miles east of the accident site. The 1353 weather observation from the Palmer Airport was reporting, in part: Wind, 140 degrees (true) at 16 knots, gusting to 21 knots; visibility, 10 statute miles; clouds and sky condition, 4,000 scattered, 7,000 feet broken, 9,000 overcast; temperature, 55 degrees F; dew point, 33 degrees F; altimeter, 29.77 inches Hg. According to a carburetor icing probability chart, the conditions at the time of the accident were conducive to serious carburetor icing at any engine power setting. No preaccident mechanical problems were reported, and due to the remote location, the airplane and engine were not examined by the NTSB. During takeoff from a lake in a float-equipped airplane, the pilot said the airplane became airborne, but the engine began to lose power. The pilot said that he did not think the airplane would clear the trees at the end of the lake, so he started a right turn to stay over the water. As he steepened the turn, the airplane stalled and impacted the lake. The pilot said the outside temperature was about 55 degrees Fahrenheit and that it was raining. He reported that the more he thought about the circumstances, the more he believed that the loss of power was the result of carburetor ice. The weather conditions at the time of the accident were conducive to serious icing conditions at any engine power setting. No preaccident mechanical problems that would have precluded normal operation were reported. 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-Contributed to outcome - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2012_ANC12LA096.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, stall, turbulence). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2023 · Faculty research project
Understanding the Coupled Interactions Between Hair-Like Micromechanoreceptors and Wall Turbulence
This research focuses on understanding the interactions between turbulent flows and long (high aspect ratio), flexible hair-like microstructures or micropillars inspired by those encountered in nature…
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA)
Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint
Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Aerodynamic prediction of glaze ice accretion on airfoils and wing is studied using the Reynolds-averaged Navier-Stokes method.
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
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