NTSB CAROL · Event
Event CEN14CA162
Registry · N242JB
FAA Aircraft Registry record.
Make / Model
BEECH 35-C33A
Year of manufacture
1966 · 48 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19660427
ADS-B equipped
Yes — Mode-S A23837
Registrant of record
MCGREGOR TODD R
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A loss of aircraft control during landing, due to the pilot's excessive braking. Contributing to the accident was the pilot's lack of recent flight experience.
Factual narrative
The pilot stated that as he applied brakes after touchdown, the wheels locked up and the airplane began to skid. The airplane departed the left side of the runway and impacted runway lighting obstructions near the intersection of the runway and a taxiway. The pilot stated that he lost control of the airplane due to a lack of recent flight experience, as well as his excessive braking actions, due to recent installation of new brake pads. The pilot had not flown an airplane for over five months prior to the accident. The pilot stated that as he applied brakes after touchdown, the wheels locked up and the airplane began to skid. The airplane departed the left side of the runway and impacted runway lighting obstructions near the intersection of the runway and a taxiway. The pilot stated that he lost control of the airplane due to a lack of recent flight experience, as well as his excessive braking actions, due to recent installation of new brake pads. The pilot had not flown an airplane for over five months prior to the accident. 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Surface speed/braking-Incorrect use/operation - C
- F Personnel issues-Experience/knowledge-Experience/qualifications-Recent experience-Pilot - F
- — Environmental issues-Physical environment-Object/animal/substance-Runway/taxi/approach light-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2014_CEN14CA162.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 (stall). 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 · 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…
Browse the full corpus — academia portal ↗