ANC07LA096
2007-09-07 · Anchorage, Alaska, United States · None · 1 aircraft · Status: Completed
Airport PALH
Aircraft involved
Probable cause & findings
A loss of engine power for an undetermined reason.
Factual narrative
On September 7, 2007, about 1640 Alaska daylight time, a float-equipped Cessna 185 airplane, N1758R, sustained substantial damage when it collided with the water and beach of Lake Spenard, during an emergency landing after takeoff from the Lake Hood Seaplane Base, Anchorage, Alaska. The airplane was being operated as a visual flight rules (VFR) local area personal flight under Title 14, CFR Part 91, when the accident occurred. The airplane was operated by the pilot. The airline transport certificated pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed, and no flight plan was filed. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on September 8, the pilot reported that during initial climb after takeoff from the southeast waterlane at Lake Hood, he noticed that the engine rpm was decreasing, and the manifold pressure was increasing. The airplane attained about 400 feet agl, but did not continue to climb. He said the airplane began to descend, and he turned toward the east to avoid a building. Emergency engine failure procedures failed to restore power, and the pilot turned sharply and descended toward Lake Spenard, leveling the airplane as it collided with the edge of the lake. During the impact, the floats were crushed upward, and the wings were displaced downward. A postaccident examination of the airplane and engine was done on September 10. No mechanical malfunction was observed during the examination. On September 13, the engine was placed on an engine test stand at an Anchorage engine overhaul facility. The engine attained full rated rpm on the test stand. The airline transport pilot was departing a lake in a float-equipped airplane. During the takeoff initial climb, the engine rpm began decreasing, and the manifold pressure was increasing. The airplane attained about 400 feet agl, but did not continue to climb. Emergency engine failure procedures failed to restore power, and the pilot turned sharply to avoid a building. He leveled the airplane just before impact along the shore of the lake. A postaccident examination of the airplane and engine found no mechanical malfunction. The engine was placed on an engine test stand where it attained full rated rpm. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_ANC07LA096.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 (engine failure). All research papers
- arXiv 2022 · arXiv preprint Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM) A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum) Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…