ERA14CA191
2014-04-05 · La Belle, Florida, United States · Minor · 1 aircraft · Status: Completed
Airport X14
Current FAA registration · N410KT
- Make / Model
- ZENITH ZENITH CH 701
- Year of manufacture
- 2012 · 2 years old at event
- Engine
- CONT MOTOR C85-12F (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 20130912
- ADS-B equipped
- Yes — Mode-S A4D513
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed after a total loss of engine power at takeoff, which resulted in a hard landing. Also causal was the pilot/owner/builder's improper installation of the magnetos which resulted in the engine power loss.
Factual narrative
The pilot/owner/builder reported that at 30 to 50 feet above the runway in a steep climb after takeoff, the engine stopped producing power. The airplane "nosed over quickly" and landed hard on the nose wheel, bounced, and landed hard on the nose wheel again, collapsing it, and causing substantial damage to the firewall and airframe. Examination of the airplane's engine by an FAA airworthiness inspector revealed that both magnetos were improperly grounded at installation. The installation as found resulted in a degraded performance, and over time, resulted in a complete ignition failure and total loss of engine power. The pilot/owner/builder reported that at 30 to 50 feet above the runway in a steep climb after takeoff, the engine stopped producing power. The airplane "nosed over quickly" and landed hard on the nose wheel, bounced, and landed hard on the nose wheel again, collapsing it, and causing substantial damage to the firewall and airframe. Examination of the airplane's engine by an FAA airworthiness inspector revealed that both magnetos were improperly grounded at installation. The installation as found resulted in a degraded performance, and over time, resulted in a complete ignition failure and total loss of engine power. 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-Airspeed-Not attained/maintained - C
- C Personnel issues-Task performance-Maintenance-Installation-Owner/builder - C
- — Aircraft-Aircraft power plant-Ignition system-Magneto/distributor-Incorrect service/maintenance
Verbatim from NTSB's published report. Source file
NTSB_2014_ERA14CA191.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 ↗
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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…