CEN14CA402
2014-07-29 · Pine Bluff, Arkansas, United States · None · 1 aircraft · Status: Completed
Airport PBF
Current FAA registration · N9836H
- Make / Model
- CESSNA 182R
- Year of manufacture
- 1981 · 33 years old at event
- Engine
- CONT MOTOR O-470 SERIES (230 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19811001
- ADS-B equipped
- Yes — Mode-S ADB97B
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The inadvertent aerodynamic stall during landing in crosswind conditions.
Factual narrative
The pilot stated that he was in the traffic pattern about 700 feet higher than normal and intended to make a short field landing to runway 36. He turned onto the final approach, reduced the throttle to idle, extended flaps, and trimmed the airplane for 60 knots. The pilot crabbed the airplane into the wind which he noted to be from 060 degrees at 11 knots. Just prior to touchdown he applied left rudder to align the nose of the airplane with the runway. A gust of wind raised the right wing and the airplane landed hard. After landing, he taxied the airplane to a hangar on the airfield. The airplane sustained substantial damage to the firewall. The pilot later stated that the airplane stalled during landing when the right wing was raised. The pilot stated that he was in the traffic pattern about 700 feet higher than normal and intended to make a short field landing to runway 36. He turned onto the final approach, reduced the throttle to idle, extended flaps, and trimmed the airplane for 60 knots. The pilot crabbed the airplane into the wind which he noted to be from 060 degrees at 11 knots. Just prior to touchdown he applied left rudder to align the nose of the airplane with the runway. A gust of wind raised the right wing and the airplane landed hard. After landing, he taxied the airplane to a hangar on the airfield. The airplane sustained substantial damage to the firewall. The pilot later stated that the airplane stalled during landing when the right wing was raised. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2014_CEN14CA402.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…