NTSB CAROL · Event
Event ERA11CA045
Registry · N611TX
FAA Aircraft Registry record.
Make / Model
DASSAULT AVIATION FALCON 900EX
Year of manufacture
2005 · 5 years old at event
Engine
HONEYWELL TFE731-60-1C
Seats / Engines
21 seats · 3 engines
Last airworthiness date
20180419
ADS-B equipped
Yes — Mode-S A7F434
Registrant of record
MEGAEQUIPMENT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper recovery from a bounced landing and the certificated flight instructor's inadequate remedial action, which resulted in an aerodynamic stall during a go-around.
Factual narrative
According to the flight instructor, he was giving flight instruction to another pilot who was not rated in special light sport weight-shift airplanes. The pilot receiving instruction was flying the airplane at the time of the accident from the front seat, with the flight instructor in the rear seat. Upon landing, the airplane bounced and when the flight instructor called for a go-around, the pilot receiving instruction pushed the control bar "out too far," causing the airplane to stall. The stall caused the airplane to roll to the left, touch the left wingtip to the ground, and the airplane cartwheeled. The flight instructor stated that the pilot receiving instruction had more leverage than the rear seat pilot's "instructor bars." Postaccident examination by a Federal Aviation Administration inspector revealed substantial damage to the entire fuselage. According to the certificated flight instructor (CFI), he was giving instruction to another pilot who was not rated in special light sport weight-shift airplanes. During touchdown, the airplane bounced and the CFI instructed the pilot undergoing instruction (PUI) to perform a go-around. The PUI pushed the control bar and the airplane stalled. The airplane to roll to the left and the left wingtip contacted the ground, resulting in the airplane tumbling in a cartwheel-type movement. The CFI stated that the PUI was seated in the rear seat and therefore had more leverage than his controls. Postaccident examination by a Federal Aviation Administration inspector revealed damage was sustained to fuselage structure. 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 Personnel issues-Action/decision-Action-Incomplete action-Instructor/check pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA11CA045.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.
- Embry-Riddle Scholarly Commons 2024 · Conference paper
Green Skies Over Akron: “Revolutionizing CAK with a $20M Sustainability Blueprint"
Our groundbreaking research at Akron-Canton Airport (CAK) proposes a transformative $20 million electrical master plan, designed to revolutionize the airport into a sustainable aviation hub and an Adv…
- Embry-Riddle Scholarly Commons 2022 · Conference paper
Industry Panel - Workplace Diversity, Equity, and Inclusion (DE&I) Revolution: From Talk to Collective Action
Panelists will discuss initiatives in the workplace, lessons learned, and resources for people and organizations to take action at work and in the community.
- NASA NTRS 2018 · Other
Compressor Stall Recovery Through Tip Injection Assessed
Aerodynamic stability is a fundamental limit in the compressor design process. The development of robust techniques for increasing stability has several benefits: enabling higher loading and fewer bla…
- 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…
Browse the full corpus — academia portal ↗