NTSB CAROL · Event
Event SEA96LA210
Registry · N2595N
FAA Aircraft Registry record.
Make / Model
CESSNA 120
Year of manufacture
1947 · 49 years old at event
Engine
CONT MOTOR C85 SERIES (85 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19550506
ADS-B equipped
Yes — Mode-S A27C01
Registrant of record
NAMPA TAILDRAGGER FLYING CLUB INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the solo student pilot's failure to maintain directional control of the airplane during the landing roll, which resulted in a ground loop/swerve.
Factual narrative
On September 4, 1996, about 0745 mountain daylight time, N2595N, a Cessna 120, operated by the Nampa Taildraggers Flying Club, Nampa, Idaho, groundlooped during landing in Nampa and was substantially damaged. The student pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed and no flight plan had been filed. The local instructional flight was conducted under 14 CFR 91. According to an eyewitness (statement attached): "[The] aircraft touched down and started porpoising. It looked like he was about to get the aircraft under control, but then it turned left and groundlooped off the left side of the runway." According to an FAA aviation safety inspector from Boise, Idaho, the student pilot lost directional control during landing, swerved off the runway, and collided with rough terrain. No preimpact mechanical malfunctions were reported by the pilot or the inspector. The student pilot had accumulated a total of 48 hours of flying time in the Cessna 120. Calm wind conditions were reported at the time of the accident. The student pilot, the sole occupant, was practicing landings in a tail-wheel equipped airplane. During one of the landings, the airplane veered off the left side of the runway into rough terrain and was substantially damaged. No preimpact mechanical malfunction was reported by the pilot, nor was any found during the investigation. The student pilot had accumulated a total of 48 hours of flying time in the Cessna 120. Calm wind conditions were reported at the time of the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_SEA96LA210.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.
- arXiv 2024 · arXiv preprint
Mechanisms of de-icing by surface Rayleigh and plate Lamb acoustic waves
Acoustic waves (AW) have recently emerged as an energy-efficient ice removal procedure compatible with functional and industrial-relevant substrates.
- 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…
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