GAA19CA247
2019-05-06 · Auburn, California, United States · None · 1 aircraft · Status: Completed
Airport AUN
Aircraft involved
Probable cause & findings
The pilot's improper retraction of the flaps during a go-around and his exceedance of the airplane’s critical angle of attack, which resulted in an aerodynamic stall.
Factual narrative
The solo student pilot reported that, he simulated a power-off emergency landing with a 180º turn to the runway and trimmed the elevator "fully nose up" and added full flaps. Prior to touchdown, the airplane drifted right of centerline and he had "difficulty correcting and maintaining control" of the airplane so he initiated a go around. Subsequently, the student "retracted flaps entirely" and the airplane "fell [about 10 ft] to the ground," the nose wheel impacted the terrain and the airplane nosed over. The airplane sustained substantial damage to the left wing and empennage. The student reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The automated weather observation station located on the airport reported that, about the time of the accident, the wind was from 220° at 6 knots. The student was landing the airplane on runway 25. The solo student pilot reported that he simulated a power-off emergency landing with a 180º turn to the runway and then trimmed the elevator "fully nose up" and added full flaps. Before touchdown, the airplane drifted right of centerline, and he had "difficulty correcting and maintaining control" of the airplane, so he initiated a go-around. The student added that, subsequently, he "retracted [the] flaps entirely," and the airplane "fell [about 10 ft] to the ground," the nosewheel impacted terrain, and the airplane then nosed over. The airplane sustained substantial damage to the left wing and empennage. The student reported that there were no preaccident mechanical failures or malfunctions 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Configuration-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA247.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…