GAA19CA212
2019-04-17 · Wickenburg, Arizona, United States · Minor · 1 aircraft · Status: Completed
Airport E25
Current FAA registration · N425PA
- Make / Model
- PIPER PA-28-181
- Year of manufacture
- 2001 · 18 years old at event
- Engine
- LYCOMING 0-360-A1D (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20010720
- ADS-B equipped
- Yes — Mode-S A50F78
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain lateral control during landing and his exceedance of the airplane’s critical angle of attack during the subsequent aborted landing, which resulted in an aerodynamic stall.
Factual narrative
The student pilot reported that, on his second approach, he encountered "bumpy" air and the aircraft ballooned. He corrected by adding power, leveling the wings and continuing the landing. Just prior to touching down, the right wing raised, and the airplane drifted to the left. He applied power to go-around, the stall warning activated but the airplane continued to drift left. Subsequently, the airplane aerodynamically stalled and collided with the ground. Per the photos provided by the Federal Aviation Administration that the airplane also impacted an airport taxi way sign during the accident. The airplane sustained substantial damage to the left wing and fuselage. The student pilot reported that there were no preimpact mechanical failures or malfunctions with the airplane that would have precluded normal operation. About the time of the accident, the automated weather reporting station located at the airport, reported that the wind was from 270° at 6 knots. The pilot was landing the airplane on runway 23. The student pilot reported that, on his second approach, he encountered "bumpy" air, and the airplane ballooned. He corrected by adding power, leveling the wings, and continuing the landing. Just before touchdown, the right wing lifted, and the airplane drifted left of the runway centerline. He applied power to go around, but the stall warning activated, and the airplane continued to drift left. Subsequently, the airplane aerodynamically stalled and collided with the ground and an airport taxiway sign. The airplane sustained substantial damage to the left wing and fuselage. The student reported that there were no preimpact mechanical failures or malfunctions with the airplane that would have precluded normal operation. About the time of the accident, the airport's automated weather reporting station reported that the wind was from 270° at 6 knots. The pilot was landing the airplane on runway 23. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Not attained/maintained - C
- — Environmental issues-Physical environment-Object/animal/substance-Sign/marker-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA212.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
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Related research
Matched on aircraft type or causal vocabulary (stall, go-around). All research papers
- 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…