ERA24LA312
2024-07-21 · Rural Retreat, Virginia, United States · None · 1 aircraft · Status: Completed
Airport MKJ
Current FAA registration · N185GS
- Make / Model
- CESSNA A185F
- Year of manufacture
- 1978 · 46 years old at event
- Engine
- CONT MOTOR IO 520 SERIES (285 hp)
- Seats / Engines
- 6 seats · 1 engine
- Last airworthiness date
- 19780724
- ADS-B equipped
- Yes — Mode-S A153E6
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A loss of directional control during the landing roll.
Factual narrative
The pilot of the tailwheel-equipped airplane reported that after completing a short cross-country flight, he entered the airport pattern for a full-stop landing. The pilot described that he configured the airplane up for a “full stall, 3-point landing” and upon touching down, the airplane “abruptly swerved to the right.” The pilot recounted that it felt “as if the right brake was applied” but reported that both of his feet were off the brakes. The pilot applied left brake, but it was ineffective because the left wheel was pulled off the runway by the abrupt swerve to the right. To compensate, the pilot increased throttle input, which inadvertently resulted in the airplane beginning a climb away from the runway before entering a descending left turn. Following the accident, a Federal Aviation Administration inspector examined the airplane’s wheels, tires, and brakes, and found no evidence of any anomalies. A subsequent detailed inspection of the right brake by a mechanic revealed that the internal components of the brake had little wear and showed no evidence of damage or defects. The left main landing gear separated from the fuselage during the accident sequence, therefore the integrity of the hydraulic system used to actuate the brake could not be evaluated. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2024_ERA24LA312.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 ↗
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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…