ERA20CA239
2020-07-02 · Crystal River, Florida, United States · None · 1 aircraft · Status: Completed
Airport CGC
Aircraft involved
Probable cause & findings
The flight instructor's delayed remedial action during a simulated engine failure on takeoff, which resulted in a loss of directional control.
Factual narrative
The flight instructor was conducting a training flight with the private pilot in the multiengine airplane. The flight instructor said that shortly after the airplane began to accelerate down the runway, she pulled the left throttle to idle to simulate an engine failure on takeoff and the private pilot "froze." She told him to bring the engine power to idle and brake, which he did, but the airplane was already veering left. The flight instructor then took control of the airplane and shut off power to each engine, but the airplane exited the runway and impacted an embankment resulting in substantial damage to the fuselage. The private pilot said that he responded to the simulated engine failure by removing thrust on both engines, applying the brakes, and trying to maintain directional control; however, "Despite the measures taken, the plane skidded off the runway." The flight instructor reported that there were no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The flight instructor was conducting a training flight with the private pilot in the multiengine airplane. The flight instructor said that shortly after the airplane began to accelerate down the runway, she pulled the left throttle to idle to simulate an engine failure on takeoff and the private pilot "froze." She told him to bring the engine power to idle and brake, which he did, but the airplane was already veering left. The flight instructor then took control of the airplane and shut off power to each engine, but the airplane exited the runway and impacted an embankment resulting in substantial damage to the fuselage. The private pilot said that he responded to the simulated engine failure by removing thrust on both engines, applying the brakes, and trying to maintain directional control; however, "Despite the measures taken, the plane skidded off the runway." The flight instructor reported that there were no preimpact mechanical malfunctions 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot
Verbatim from NTSB's published report. Source file
NTSB_2020_ERA20CA239.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- NTSB Aircraft Accident Reports 2018 · Accident report Atlas Air Flight 3591 Boeing 767 Loss of Control (preliminary)
Atlas Air 3591 / Boeing 767-300 / Trinity Bay TX (Feb 23 2019) — preliminary. Preliminary investigation findings; superseded by the AAR-21/01 final report.
- NTSB Aircraft Accident Reports 2021 · Accident report Crash of Atlas Air Flight 3591, Boeing 767-300 (N1217A)
Atlas Air 3591 crashed into Trinity Bay, Texas, February 23, 2019. Investigation of the in-flight loss-of-control crash of Atlas Air 3591 into Trinity Bay, Texas.
- 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.