NTSB CAROL · Event
Event ERA19TA277
Registry · N12033
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-6
Year of manufacture
1995 · 24 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19960824
ADS-B equipped
Yes — Mode-S A0568F
Registrant of record
ECHEVERRI OTTO
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s inability to maintain control due to passenger interference.
Factual narrative
On September 23, 2019, about 1157 eastern daylight time, an experimental, amateur-built RV-6, N12033, sustained substantial damage when it was involved in an accident near Lakeland, Florida. The pilot received serious injuries; the passenger was uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot, who was also a flight instructor, stated that the airplane owner contacted him for tailwheel instruction in his recently-purchased RV-6. The owner did not hold a pilot certificate, but the pilot agreed to fly the airplane with the owner as a passenger. The pilot performed a preflight inspection with no anomalies noted and departed on a local flight before returning to the airport. The pilot performed one go-around due to a crosswind, and during the subsequent landing approach, “the airplane banked to the left and pitch[ed] down about 8 or 10 degrees.” The pilot attempted to regain control of the airplane, but the controls were “very stiff.” He recalled heading toward the trees and tried again to move the controls; this time, the airplane pitched up slightly, but not enough to slow the descent. The airplane impacted trees and the ground, resulting in substantial damage to the fuselage, wings, and empennage. The pilot reported that he thought the passenger applied control inputs to maneuver the airplane during landing, which resulted in his inability to control the airplane. He stated that the airplane “definitely did not stall.” He also reported that the airplane had no preimpact mechanical malfunctions or failures that would have precluded normal operation. The owner of the airplane did not provide a statement regarding the accident. Examination of the airplane by a Federal Aviation Administration (FAA) inspector confirmed flight control continuity from the cockpit controls to the elevator and ailerons. The pilot, who was also a flight instructor, stated that the airplane owner contacted him for tailwheel instruction in his recently purchased airplane. The owner did not hold a pilot certificate, but the pilot agreed to fly the airplane with the owner as a passenger. The pilot stated that, during landing approach, “the airplane banked to the left and pitch[ed] down about 8 or 10 degrees.” The pilot attempted to regain control of the airplane, but the controls were “very stiff.” He recalled heading toward the trees and tried again to move the controls; this time, the airplane pitched up slightly, but not enough to slow the descent. The airplane impacted trees and the ground, resulting in substantial damage to the fuselage, wings, and empennage. The pilot reported that he thought the passenger applied control inputs during landing, which resulted in his inability to control the airplane. He stated that the airplane “definitely did not stall.” He also reported that there were no preimpact mechanical malfunctions or failures of the airplane that would have precluded normal operation. The owner of the airplane did not provide a statement regarding 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).
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained
- — Personnel issues-Action/decision-Action-Incorrect action performance-Passenger
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2019_ERA19TA277.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, go-around). 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
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