NTSB CAROL · Event
Event ANC98LA030
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for crosswind conditions during landing. A factor was the crosswind.
Factual narrative
On March 24, 1998, about 1045 Alaska standard time, a wheel equipped Cessna 185E airplane, N1987U, sustained substantial damage while landing at Merrill Field, Anchorage, Alaska. The airplane was being operated as a visual flight rules (VFR) local area flight under Title 14 CFR Part 91 when the accident occurred. The solo commercial pilot was not injured. Visual meteorological conditions prevailed. No flight plan was filed. The flight originated at Merrill Field at 1010. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on March 24, 1998 at 1100, the pilot reported that he was practicing touch-and-go landings on runway 06, which required a correction for a left cross wind. The pilot stated that on the accident landing, the airplane bounced slightly and settled onto the right main tire. The right main wheel "grabbed" as it made contact with the runway, and the airplane ground looped to the left. During the ground loop, the right wing, aileron, and right elevator struck the runway and sustained substantial damage. Merrill Field weather observation at the time of the accident consisted of: Sky conditions and ceiling, 5,500 broken, 9,000 overcast; visibility, 10 statute miles; wind, 016 degrees (magnetic) at 7 knots. The pilot noted in his written report to the NTSB that there were no preaccident mechanical anomalies with the airplane. The pilot was practicing touch-and-go landings on runway 6 in a tailwheel-equipped airplane on the paved runway. Wind conditions at the time of the accident were 016 at 7 knots. The pilot stated that the airplane bounced slightly and settled onto the right main tire. The right main wheel 'grabbed' as it made contact with the runway, and the airplane ground looped to the left. During the ground loop, the right wing, aileron, and right elevator struck the runway and sustained substantial damage. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_ANC98LA030.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 (icing). 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 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗