NTSB CAROL · Event
Event GAA19CA242
Aircraft involved
Probable cause & findings
The pilot's steep bank turn at low altitude, which resulted in a rapid descent and hard landing.
Factual narrative
The pilot reported that, during a biennial flight review, he was briefed by the flight instructor to expect a simulated engine failure during takeoff and an engine-out approach to a perpendicular runway. He departed runway 21, and about 400 ft above ground, reduced power and turned left for the dirt runway 12. He overshot the dirt runway, banked to 40°, and felt a "strong sink." He leveled the wings and added full power about 150 to 200 ft, but the airplane continued to descend. The instructor stated he considered taking the flight controls, but the pilot maintained control. The airplane landed hard, the right main landing gear struck a "rabbit hole", the airplane veered right, and the left main landing gear separated. The airplane sustained substantial damage to the fuselage. The pilot 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 about 26 miles to the east reported that, about 4 minutes before the accident, the wind was from 220° at 10 knots, temperature 72°F, dew point 34°F, altimeter setting 29.79" Hg. The pilot reported that the wind was variable at 5 to 15 knots, gusting to greater than 15 knots, temperature 80°F. The pilot added that there was severe windshear and, later in the day, the assistant airport manager reported observing a dust devil over the accident site. The pilot reported that, during a biennial flight review, the flight instructor told him to expect a simulated engine failure during takeoff and an engine-out approach to a perpendicular runway. After departure and about 400 ft above ground level (agl), the instructor reduced power, and the pilot turned left to land on the perpendicular runway. He overshot the runway, banked to 40°, and felt a "strong sink." He leveled the wings and added full power about 150 to 200 ft agl, but the airplane continued to descend. The instructor stated he considered taking the flight controls, but the pilot maintained control. The airplane landed hard, the right main landing gear (MLG) struck a hole, the airplane veered right, and the left MLG separated. The airplane sustained substantial damage to the fuselage. The pilot 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
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Lateral/bank control-Incorrect use/operation - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA242.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 (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
Browse the full corpus — academia portal ↗