WPR20CA041
2019-12-05 · Camas, Washington, United States · None · 1 aircraft · Status: Completed
Airport 1W1
Current FAA registration · N52458
- Make / Model
- CESSNA 182P
- Engine
- CONT MOTOR O-470 SERIES (230 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19731205
- ADS-B equipped
- Yes — Mode-S A69AF2
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's improper landing flare, which resulted in a bounced landing, and the flight instructor’s delayed remedial action and the student’s failure to relinquish control, which resulted in a runway overrun and impact with a fence.
Factual narrative
The flight instructor reported that with the student pilot on the controls for the landing, the airplane floated down the runway and eventually touched down on the first third of the runway. As the airplane bounced the second time, the instructor announced that he was assuming control of the airplane; simultaneously advancing the throttle to full. The students hand position on the throttle prevented full throttle application as the instructor attempted to gain altitude without stalling the airplane. The airplane subsequently struck a fence near the departure end of the runway. Power was reduced and the flight instructor initiated a forced landing to an open field. The airplane sustained substantial damage to the left side horizontal stabilizer. The instructor reported that there were no mechanical malfunctions or failures that would have precluded normal operation. The flight instructor reported that, with the student pilot on the controls for the landing, the airplane floated and eventually touched down about "the first third of the runway." The airplane bounced, and the instructor announced that he was assuming control of the airplane. The instructor simultaneously attempted to apply full throttle by pushing the student's hand, which was still on the throttle and prevented him from achieving full power as he attempted to gain altitude without stalling the airplane. The airplane subsequently struck a fence near the departure end of the runway, so the instructor reduced power and executed a forced landing to an open field. The airplane sustained substantial damage to the left horizontal stabilizer. The instructor reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation and that he should have assumed control of the airplane sooner. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
- C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
- C Environmental issues-Physical environment-Object/animal/substance-Fence/fence post-Effect on operation - C
Verbatim from NTSB's published report. Source file
NTSB_2019_WPR20CA041.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.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
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…