NTSB CAROL · Event
Event ANC03LA099
Registry · N11GA
FAA Aircraft Registry record.
Make / Model
ROBINSON HELICOPTER R44 II
Year of manufacture
2005
TCDS
H11NM · ROBINSON HELICOPTER CO
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20050721
ADS-B equipped
Yes — Mode-S A02A71
Registrant of record
CROSSWIND LEASING LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's selection of an unsuitable landing area, which resulted in an overrun and an on ground/water collision with terrain. A factor associated with the accident was a tailwind.
Factual narrative
On August 15, 2003, about 1300 Alaska daylight time, a float-equipped de Havilland DHC-2 airplane, N11GA, sustained substantial damage when it collided with the shoreline during landing at a remote lake, located about 56 miles southeast of King Salmon, Alaska. The commercial certificated pilot, and the four passengers, were not injured. The Title 14, CFR Part 91 business flight was operated in support of a sport fish guiding business. The flight operated in visual meteorological conditions and company flight following procedures were in effect. The flight was en route from another remote lake at the time of the accident. During a telephone conversation with the National Transportation Safety Board investigator-in-charge (IIC) on August 18, the pilot related that he was attempting to land on a small lake, and due to terrain clearance, a downwind approach was required. The pilot estimated the wind to be about 5 to 7 knots. He said that just after landing, he determined that he would not be able to stop the airplane before reaching the shoreline, so he applied full left rudder in an attempt to avoid the collision with the shore. He reported that during the turn, as the airplane came off of the step, the airplane's right float struck the shore. The airplane sustained structural damage to the right wing, and right wing lift strut. The pilot reported that there were no preaccident mechanical anomalies with the airplane. Neither the operator, nor the pilot, submitted an NTSB Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2). The certificated commercial pilot was landing a float-equipped airplane on a small lake, and due to terrain clearance, a downwind approach was required. The pilot estimated the wind to be about 5 to 7 knots. Just after landing, he determined that he would not be able to stop the airplane before reaching the shoreline, so he applied full left rudder in an attempt to avoid the collision with the shore. During the turn, as the airplane came off of the step, the airplane's right float struck the shore. The airplane sustained structural damage to the right wing, and right wing lift strut. The pilot reported that there were no preaccident mechanical anomalies with the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_ANC03LA099.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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