ANC10LA019
2010-02-17 · Kwigillingok, Alaska, United States · None · 1 aircraft · Status: Completed
Airport GGV
Current FAA registration · N207DR
- Make / Model
- CESSNA 207A
- Seats / Engines
- 7 seats · 1 engine
- Last airworthiness date
- 19761229
- ADS-B equipped
- Yes — Mode-S A1AC5F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's decision to take off with ice-contaminated wings in freezing rain and mist, which resulted in an aerodynamic stall.
Factual narrative
On February 17, 2010, at 1657 Alaska standard time, a Cessna 208B, N207DR, sustained substantial damage during impact with terrain following takeoff from Kwigillingok Airport (GGV), Kwigillingok, Alaska. The airline transport pilot and his seven passengers were not injured. Grant Aviation, Anchorage, Alaska, was operating the aircraft under the provisions of 14 Code of Federal Regulations Part 135. Visual meteorological conditions prevailed for the flight, which was originating at the time of the accident. The intended destination was Kipnuk, Alaska, and a company flight plan had been filed. The pilot said that the takeoff was normal, but at 200 feet above the ground and in a turn, he observed a reduction in power. He moved the emergency fuel control lever forward, and power was restored. Before the sink rate could be reversed, the airplane impacted the surface of a frozen lake, and 5 feet of the outboard right wing was bent up. The aileron was not damaged. For safety reasons, the pilot chose to fly straight ahead for 8 miles to Kongiganak, Alaska, where the flight landed without further difficulty. The operator's maintenance personnel inspected the engine and airframe, and determined that the right wing required a major repair to restore it to an airworthy condition. After a field repair of the right wing by the operator, the Federal Aviation Administration (FAA) granted a ferry permit for a one time flight from Kongiganak to Anchorage. The operator found no discrepancies with the engine, and it operated normally during the ferry flight. The pilot reported to a FAA inspector that the cloud condition was 500 feet overcast with 2.5 miles visibility in light snow. There was a light wind from the north at approximately 3 to 5 knots. When the inspector asked the pilot if the airplane had ice on it when it departed Kwigillingok, he stated that there was a "trace" of ice on the wings. When interviewed by the FAA inspector, passengers made the following statements: 1. "There was freezing rain." 2. "The plane was iced up and when it took off it stalled." 3. "The weather was icing rain….There was some ice on the wings before they took off from Kwigillingok." There was no weather reporting facility at Kwigillingok. The closest weather reporting station was at Kipnuk, Alaska, about 26 nautical miles west of the accident site. At 1656, the reported conditions were: wind 050 degrees at 7 knots; visibility 10 statute miles; cloud condition, broken at 400 feet, overcast at 3,300 feet; temperature 23 degrees Fahrenheit; dew point 23 degrees Fahrenheit; altimeter setting 29.67 inches of Mercury. The pilot told the National Transportation Safety Board's (NTSB) investigator-in-charge that the cloud condition was an indefinite ceiling at 500 to 600 feet with light snow, and the temperature was 30 degrees Fahrenheit. An NTSB meteorologist did a weather study and found that the area was subject to light snow showers, freezing fog and mist, and ground temperatures were below freezing. The limitations section of the Cessna 208B flight manual supplement "Known Icing Equipment," states, in part: "Takeoff is prohibited with any frost, ice, snow, or slush adhering to the wings, horizontal stabilizer, vertical stabilizer, control surfaces, proper blades, or engine inlets." The limitations section also includes the following: "WARNING, EVEN SMALL AMOUNTS OF FROST, ICE, SNOW OR SLUSH ON THE WING MAY ADVERSELY CHANGE LIFT AND DRAG. FAILURE TO REMOVE THESE CONTAMINANTS WILL DEGRADE AIRPLANE PERFORMANCE AND MAY PREVENT A SAFE TAKEOFF AND CLIMBOUT." Passengers reported that prior to departing on the accident flight they observed ice on the wings and described the weather as foggy, with freezing rain. Shortly after takeoff, at an estimated 200 feet above the ground, the pilot reported a series of power fluctuations, coinciding with a loss of altitude. The pilot stated that he engaged the emergency power lever, and that power was restored, but not before the airplane collided with a frozen lake, damaging the right wing. The airplane subsequently became airborne, and the pilot elected to fly to another village to land. A postaccident inspection disclosed no mechanical anomalies with the engine or its accessories, and the airplane was flown to its base after the wing was repaired without any engine problems noted. A weather study by a Safety Board meteorologist determined that the area was subject to light snow showers, freezing fog and mist, and surface temperatures below freezing, all conducive to wing/airframe icing. During an interview with Federal Aviation Administration inspectors, the pilot acknowledged seeing “a trace of ice” on the wings. The limitations section of the airplane's flight manual supplement "Known Icing Equipment," states, in part: "Takeoff is prohibited with any frost, ice, snow, or slush adhering to the wings, horizontal stabilizer, vertical stabilizer, control surfaces, proper blades, or engine inlets." The limitations section also includes the following: "WARNING, EVEN SMALL AMOUNTS OF FROST, ICE, SNOW OR SLUSH ON THE WING MAY ADVERSELY CHANGE LIFT AND DRAG. FAILURE TO REMOVE THESE CONTAMINANTS WILL DEGRADE AIRPLANE PERFORMANCE AND MAY PREVENT A SAFE TAKEOFF AND CLIMBOUT." Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
- C Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-Conducive to structural icing-Decision related to condition - C
- — Aircraft-Aircraft structures-Wing structure-(general)-Damaged/degraded
Verbatim from NTSB's published report. Source file
NTSB_2010_ANC10LA019.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (icing, stall, maintenance). All research papers
- Embry-Riddle Scholarly Commons 2023 · Faculty research project Reconfigurable Guidance and Control Systems for Emerging On-Orbit Servicing, Assembly, and Manufacturing (OSAM) Space Vehicles
Dynamic response to emergent situations is a necessity in the on-orbit servicing, assembly, and manufacturing (OSAM) field, because traditional on-orbit guidance and control (G&C) cannot respond effic…
- 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.
- Embry-Riddle Scholarly Commons 2023 · Conference paper The Value of Strong Partnerships to Build a Successful Aviation Maintenance Career Pathway Program for Transitioning Military Service Members
The aerospace industry is competing with other industries for a qualified workforce, and many of those competing industries are investing heavily in creating workforce development pipelines.
- 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…
- 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…
- NASA NTRS 2019 · Technical Publication (TP) NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …