FTW94LA111
1994-03-18 · FLIPPIN, Arkansas, United States · None · 1 aircraft · Status: Completed
Airport FLP
Current FAA registration · N6654H
- Make / Model
- CESSNA 172M
- Year of manufacture
- 1975 · 19 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19750701
- ADS-B equipped
- Yes — Mode-S A8C9B8
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE STUDENT PILOT'S PREMATURE FLARE AND THE RESULTANT INADVERTENT STALL.
Factual narrative
On March 18, 1994, at 0810 central standard time, a Cessna 172M, N6654H, was substantially damaged during landing near Flippin, Arkansas. The student pilot was not injured. Visual meteorological conditions prevailed for the solo instructional flight. In his Pilot/Operator Report and in an interview with a Federal Aviation Administration inspector, the pilot stated that on approach he initiated the flare too high and "stalled above the runway." The stall resulted in a "hard landing" damaging the airframe and fire wall. THE STUDENT PILOT FLARED TOO HIGH AND STALLED THE AIRPLANE ABOVE THE THRESHOLD. SUBSEQUENTLY LANDED HARD DAMAGING THE AIRFRAME AND FIREWALL. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_FTW94LA111.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- 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…