NTSB CAROL · Event
Event CEN25LA404
Registry · N814
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR20
Year of manufacture
2003 · 22 years old at event
Engine
CONT MOTOR IO-360 SER (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20030130
ADS-B equipped
Yes — Mode-S AB1837
Registrant of record
WISCONSIN AVIATION-FOUR LAKES INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor’s failure to maintain control of the airplane following the student pilot’s bounced landing. Contributing to the accident was the flight instructor’s delayed remedial action which resulted in diminished airplane performance during the go-around.
Factual narrative
The flight instructor and student pilot were conducting a primary instruction flight. The flight instructor reported that the surface wind was calm as they approached the airport to land. The flight instructor stated that the student pilot allowed the airplane to be “slightly high and fast” while on short final approach, but the airplane then joined a normal descent path as it continued toward the runway. The flight instructor estimated that the airplane was 5-10 knots faster than a normal landing speed as it flew over the runway identification numbers. At that point, the flight instructor told the student to reduce engine power to idle, transition his sight picture down the runway, and allow the airplane to decelerate during the landing flare. The airplane bounced upon touchdown, ballooned, descended, and then bounced a second time before the flight instructor took control of the airplane from the student pilot. The flight instructor then increased engine power, increased right rudder input, and pitched for a level attitude to increase airspeed for a go-around. The airplane did not accelerate and bounced for a third time, this time with the stall warning horn audible. The flight instructor reduced the wing flaps from 100% to 50% to gain additional airspeed while flying in ground effect, but she noted that the airplane had ineffective roll and yaw control. She reduced engine power to idle as the airplane drifted left, struck a runway edge light, and departed off the left side of the runway. The airplane then entered an area of high vegetation where it spun around to a stop. The airplane’s aft fuselage sustained substantial damage during the accident. The flight instructor did not report any preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. 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-Pitch control-Not attained/maintained
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Lateral/bank control-Not attained/maintained
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Yaw control-Not attained/maintained
- — Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Instructor/check pilot
Verbatim from NTSB's published report. Source file
NTSB_2025_CEN25LA404.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…
Browse the full corpus — academia portal ↗