NTSB CAROL · Event
Event ANC01LA121
Registry · N10395
FAA Aircraft Registry record.
Make / Model
DEHAVILLAND BEAVER DHC-2
Year of manufacture
1959 · 42 years old at event
Engine
P&W R-985 SERIES (450 hp)
Seats / Engines
8 seats · 1 engine
Last airworthiness date
19980828
ADS-B equipped
Yes — Mode-S A0138A
Registrant of record
FLYWAYS NORTH LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for gusty wind conditions. Factors associated with the accident were the pilot's inadequate weather evaluation, and wind gusts.
Factual narrative
On August 21, 2001, about 1430 Alaska daylight time, a float-equipped de Havilland DHC-2 airplane, N10395, sustained substantial damage during takeoff from Six Mile Lake, Nondalton, Alaska. The airplane was being operated as a visual flight rules (VFR) on-demand passenger flight under Title 14, CFR Part 135, when the accident occurred. The airplane was owned by Ernest M. Brooks, and operated by Alaska Air Taxi, Inc., Anchorage, Alaska. The certificated commercial pilot, and the four passengers, were not injured. Visual meteorological conditions prevailed, and company visual flight rules (VFR) flight following procedures were in effect for the flight to Port Alsworth, Alaska. During a telephone conversation with the National Transportation Safety Board investigator-in-charge on August 21, the pilot reported that just after takeoff, about 100 feet above the water, a very strong gust of wind rolled the wings of the airplane about 90 degrees to the left. He said that he applied full right aileron in an attempt to regain control, but the airplane descended, and the left wing struck the surface of the water. As the airplane's left wing struck the surface of the water, the wing separated from the fuselage, pivoted the airplane 90 degrees to the left, and the right wing stuck the water. Both floats were torn from the fuselage, and the airplane eventually sank in shallow water. The airplane sustained substantial damage to the fuselage, wings, and empennage. The pilot reported that wind conditions at the time of the accident were out of the northwest at 20 knots, with gusts to 30 knots. The certificated commerical pilot reported to the NTSB that just after takeoff, about 100 feet above the water, a very strong gust of wind rolled the wings of the float-equipped airplane about 90 degrees to the left. He said that he applied full right aileron in an attempt to regain control, but the airplane descended, and the left wing struck the surface of the water. As the airplane's left wing struck the surface of the water, the wing separated from the fuselage, pivoted the airplane 90 degrees to the left, and the right wing struck the water. Both floats were torn from the fuselage, and the airplane eventually sank in shallow water. The airplane sustained substantial damage to the fuselage, wings, and empennage. The pilot reported that wind conditions at the time of the accident were out of the northwest at 20 knots, with gusts to 30 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_ANC01LA121.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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