NTSB CAROL · Event
Event CEN12CA624
Registry · N824KS
FAA Aircraft Registry record.
Make / Model
CESSNA 172R
Year of manufacture
1999 · 13 years old at event
Engine
LYCOMING I0360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19990120
ADS-B equipped
Yes — Mode-S AB40A9
Registrant of record
PLANELEASE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor's improper flare in gusty wind conditions, which resulted in a hard landing.
Factual narrative
The certificated flight instructor (CFI) and student pilot were practicing takeoff and landings. After performing a stop-and-go on the 4,300 foot long runway, the CFI pulled the engine back to idle to demonstrate a simulated engine-out landing to the student pilot. The CFI reported that the airplane made a rapid descent from about 200 feet above ground level, he flared too high and the airplane landed hard on the runway. The CFI stated that the wind was 10 degrees from the runway heading, and gusting to 33 knots at the time. Substantial damage was sustained to the airplane's firewall. The CFI did not report any mechanical malfunctions prior to the accident. The flight instructor and student pilot were practicing takeoffs and landings. During the climb after a stop-and-go landing on the 4,300 foot long runway, the flight instructor reduced the engine power to idle to demonstrate a simulated engine-out landing to the student pilot. The flight instructor reported that the airplane made a rapid descent from about 200 feet above ground level, and then he flared too high; the airplane landed hard on the runway, substantially damaging the airplane’s firewall. The flight instructor stated that the wind at the time was from about 10 degrees left of the runway heading at 28 knots, gusting to 33 knots. The flight instructor reported no preaccident mechanical malfunctions. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Decision related to condition
Verbatim from NTSB's published report. Source file
NTSB_2012_CEN12CA624.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 ↗