NTSB CAROL · Event
Event ANC99LA071
Registry · N7560K
FAA Aircraft Registry record.
Make / Model
CESSNA 180J
Year of manufacture
1976 · 23 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19760317
ADS-B equipped
Yes — Mode-S AA32B5
Registrant of record
ALBERT BRYAN WAYNE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The failure of the pilot to maintain directional control during the water landing.
Factual narrative
On June 8, 1999, about 1700 Alaska daylight time, a float equipped Cessna 180J airplane, N7560K, sustained substantial damage during landing on Wolf Lake, Palmer, Alaska. The airline transport pilot and the one, pilot-rated passenger aboard were not injured. The airplane was being operated as a Visual Flight Rules (VFR) personal flight under 14 CFR Part 91. The flight departed from Alexander Creek, Alaska, about 1630. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The pilot told the NTSB investigator-in-charge (IIC), during an interview on June 9, that he was landing the airplane with a left crosswind. He stated that the airplane landed on the left float first. The pilot stated that when the right float touched down, the airplane swerved left. He indicated that the airplane pitched nose down, striking the right wing and propeller. The pilot did not remember hitting anything with the floats, although the right float had a one foot long crease along the keel near the forward compartment aft bulkhead. The right wing and aileron sustained substantial damage. Postaccident inspection revealed that the float struts were straight, and the lengths of the float flying wires varied by 3/4 inches. No other mechanical anomalies were noted with the airplane or floats. The floats were installed 14 hours prior to the accident. This was the second landing of the day. The pilot was landing the floatplane with a left crosswind. After touchdown on the water, the floatplane swerved left, then nosed down, damaging the right wing, right aileron, and propeller. Postaccident inspection revealed the float struts were straight, and the length of the float flying wires varied by 3/4 inch. The pilot did not remember hitting anything with the floats, but the bottom of the right float had a one foot long crease near the forward compartment. No other mechanical anomalies were noted. The floats were installed 14 hours prior to the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_ANC99LA071.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 ↗