ERA20CA146
2020-04-01 · Hollywood, Florida, United States · None · 1 aircraft · Status: Completed
Airport HWO
Aircraft involved
Probable cause & findings
The pilot’s failure to apply full engine power during the initiation of a go-around in gusting wind conditions and his exceedance of the airplane’s critical angle of attack, which resulted in an aerodynamic stall at low altitude, and the flight instructor's delayed remedial action.
Factual narrative
The flight instructor reported that during a flight review, the private pilot had completed 6 touch and go landings, in gusty wind conditions. During the subsequent approach, while the airplane was in the landing flare, a strong wind gust forced the airplane out of ground effect, and the instructor called for a go-around. The instructor reported during the go-around, the private pilot did not add full power, and he took the flight controls, however, as he did so, the airplane was already in an aerodynamic stall. Subsequently, the airplane descended, rolled to the left, and impacted the left side of the runway, where it continued into the grass and nosed over. The right wing and vertical stabilizer sustained substantial damage. The flight instructor reported that there were no mechanical malfunction or failures with the airplane that would have precluded normal operations. The flight instructor reported that, during a flight review, the private pilot completed five touch-and-go landings in gusting wind conditions. During the landing flare for the sixth touch-and-go landing, a strong wind gust forced the airplane out of ground effect, and the instructor called for a go-around. During the go-around, the pilot did not add full power, and the instructor took the flight controls; however, the airplane had already stalled. Subsequently, the airplane descended, impacted the left side of the runway, continued off the runway into grass, and nosed over. The right wing and vertical stabilizer sustained substantial damage. The instructor reported that there were no preaccident mechanical malfunction or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded - C
- C Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation - C
Verbatim from NTSB's published report. Source file
NTSB_2020_ERA20CA146.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (stall, go-around). All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- 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…