NTSB CAROL · Event
Event CEN25LA147
Registry · N6561F
FAA Aircraft Registry record.
Make / Model
CESSNA 150F
Year of manufacture
1966 · 59 years old at event
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19660217
ADS-B equipped
Yes — Mode-S A8A585
Registrant of record
WINGS AERO LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor’s failure to maintain control of the airplane during the go-around which led to the airplane exceeding its critical angle-of-attack and entering an aerodynamic stall at a low altitude. Contributing to the accident was the flight instructor’s delayed remedial action and her failure to ensure that the student had relinquished control of the airplane during the go-around.
Factual narrative
The flight instructor and student were conducting a primary instruction flight. The flight instructor reported that the student allowed the airplane to get low and slow during a landing approach. The flight instructor took control of the airplane, added full throttle for a go-around, and began to retract the flaps. The flight instructor recalled being unable to reduce airplane pitch and believed her student may have still been on the flight controls. The student reported that after the flight instructor took control of the airplane it got too slow and entered an aerodynamic stall. Airport surveillance video showed the airplane flying over the runway in a nose-high pitch attitude and yawed left when it descended and impacted the ground left wing first. The airplane then nosed over and came to rest inverted in the grass next to the runway. The airplane’s forward fuselage and vertical stabilizer were substantially damaged during the ground impact and subsequent nose over. Neither the flight instructor nor the student reported any preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. The flight instructor reported that the accident could have been prevented had she not been “overconfident” in the student’s ability to land the airplane, if she had ensured the student had relinquished control of the airplane when she began the go-around, and if she had been quicker to recognize the situation. 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-Yaw control-Not attained/maintained
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Not attained/maintained
- — Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot
- — Personnel issues-Action/decision-Info processing/decision-Identification/recognition-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_CEN25LA147.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 ↗