NTSB CAROL · Event
Event ANC95LA132
Registry · N144Q
FAA Aircraft Registry record.
Make / Model
DEHAVILLAND BEAVER DHC-2 MK.1
Year of manufacture
1961 · 34 years old at event
Engine
P&W R-985 SERIES (450 hp)
Seats / Engines
8 seats · 1 engine
Last airworthiness date
20200901
ADS-B equipped
Yes — Mode-S A0B2EA
Registrant of record
RPL AIRCRAFT LEASING LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S ABRUPT (IMPROPER) USE OF THE THROTTLE.
Factual narrative
On August 8, 1995, at 0815 Alaska daylight time, a float equipped DeHavilland DHC-2 Beaver airplane, N144Q, registered to and operated by Rainbow River Lodge, sustained substantial damage during an aborted landing at Crosswind Lake, located near the confluence of Moraine and Funnel Creeks, 40 miles south of Iliamna, Alaska. The business flight, operating under 14 CFR Part 91, departed the lodge on Lake Iliamna and the destination was Crosswind Lake. A company flight plan was in effect and visual meteorological conditions prevailed. The airline transport certificated pilot, the fishing guide, and the six passengers were not injured. During a telephone conversation with the pilot on August 10, 1995, he stated he was performing a glassy water landing and the airplane did not touchdown on the water and it "floated" approximately 1/3 of the way past the intended landing area. He applied power and the engine coughed. He stated that he applied throttle rapidly and not as smoothly as if he were applying power for a takeoff. The engine then "came to life" and he attempted to climb. The airplane would not out climb the rising terrain located in the direction of the intended flight. Examination of the engine at the accident site by an Alaska Aircraft Sales mechanic showed no reason for the engine problem. The carburetor was removed and reinstalled on the replacement engine. The ground test was normal and the subsequent flight was normal. THE PILOT WAS PERFORMING A GLASSY WATER LANDING MANEUVER ON A LAKE. THE AIRPLANE FLEW PAST THE PILOT'S INTENDED POINT OF LANDING, AND HE ABORTED THE LANDING BY RAPIDLY APPLYING POWER. THE PILOT STATED THE ENGINE COUGHED AND THEN 'CAME TO LIFE' BUT THE AIRPLANE WOULD NOT OUTCLIMB RISING TERRAIN IN THE DIRECTION OF ITS FLIGHT PATH. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_ANC95LA132.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗