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Crash of a Cessna 208B Grand Caravan in Bethel

Date & Time: Dec 18, 2007 at 0856 LT
Type of aircraft:
Operator:
Registration:
N5187B
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bethel - Hooper Bay - Scammon Bay
MSN:
208B-0270
YOM:
1991
Flight number:
CIR218
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4054
Captain / Total hours on type:
190.00
Aircraft flight hours:
12204
Circumstances:
About 0800, the commercial pilot did a preflight inspection of the accident airplane, in preparation for a cargo flight. Dark night, visual meteorological conditions prevailed. He indicated that the weather conditions were clear and cold, and frost was on the airplane. He said the frost was not bonded to the skin of the airplane, and he was able to use a broom to clean off the frost, resulting in a clean wing and tail surface. He reported that no deicing fluid was applied. After takeoff, he retracted the flaps to about 5 degrees at 110 knots of airspeed. The airplane then rolled to the right about three times in a manner he described as a wave, or vortex-like movement. He applied left aileron and lowered the flaps to 20 degrees, but the roll to the right was more severe. The pilot said the engine power was "good." He then noticed that the airplane was descending toward the ground, so he attempted to put the flaps completely down. His next memory was being outside the airplane after it collided with the ground. The airplane's information manual contains several pages of limitations and warnings about departing with even small amounts of frost, ice, snow, or slush on the airplane, as it adversely affects the airplane's flight characteristics. The manufacturer requires a visual or tactile inspection of the wings, and horizontal stabilizer to ensure they are free of ice or frost if the outside air temperature is below 10 degrees C, (50 degrees F), and notes that a heated hangar or approved deicing fluids should be used to remove ice, snow and frost accumulations. The weather conditions included clear skies, and a temperature of -11 degrees F. Post accident examination of the airplane revealed no observed mechanical malfunction. An examination of the engine revealed internal over-temperature damage, and minor external fire damage consistent with a massive spike of fuel flow at the time of ground impact. Damage to the propeller blades was consistent with high power at the time of ground impact. The rolling/vortex motion of the airplane was consistent with airframe contamination due to frost.
Probable cause:
The pilot's failure to adequately remove frost contamination from the airplane, which resulted in a loss of control and subsequent collision with terrain during an emergency landing after takeoff.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 200 in Hooper Bay

Date & Time: May 16, 1982 at 1015 LT
Operator:
Registration:
N103AQ
Survivors:
Yes
Schedule:
Bethel - Chevak - Scammon Bay - Hooper Bay
MSN:
183
YOM:
1968
Flight number:
GFF517
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4550
Captain / Total hours on type:
1990.00
Copilot / Total flying hours:
1850
Copilot / Total hours on type:
300
Aircraft flight hours:
15267
Circumstances:
The aircraft crashed while attempting to land at Hooper Bay, Alaska. The airplane crashed 1,320 feet short of the threshold of runway 13 during an approach in visual meteorological conditions. The airplane was substantially damaged when it crashed onto hard-packed snow and ice about 700 feet from the edge of the Bering Sea. There was no fire. The two pilots and six passengers sustained serious injuries in the accident.
Probable cause:
The National Transportation Safety Beard determines that the probable cause of this accident was the flightcrew's failure to compute and properly interpret the airplane's weight and balance and their operation of the airplane with the center of gravity substantially aft of its authorized limit which resulted in loss of control of the airplane during a landing attempt.
Final Report: