CEN23LA213
2023-05-20 · Ray, Michigan, United States · None · 1 aircraft · Status: Completed
Airport 57D
Current FAA registration · N586SB
- Make / Model
- PIPER PA-28-235
- Year of manufacture
- 1966 · 57 years old at event
- Engine
- LYCOMING 0-540 SERIES (250 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19670109
- ADS-B equipped
- Yes — Mode-S A78DC4
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor’s failure to maintain airplane control during simulated engine-out procedures. Contributing to the accident was the flight instructor’s decision to land with a tailwind.
Factual narrative
The flight instructor demonstrated a simulated engine failure to his student while the airplane was on the crosswind leg in the traffic pattern. He reported that he attempted to land on the opposite runway from which they departed. He reported that while maneuvering to final approach the airplane was pushed to the left of the runway over a grassy area by a “sudden downward draft.” The flight instructor stated that he thought the airplane encountered “windshear coming down between the trees.” He landed the airplane in the wet grass between the taxiway and the runway, which resulted in a propeller strike. Post-accident examination revealed substantial damage to the engine mount. The flight instructor reported that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. The flight instructor reported that the wind at the time of the accident was 300° at 10 knots. The landing was made toward runway 10 which resulted in a 9-knot tailwind. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained
- — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Effect on operation
- — Personnel issues-Action/decision-Action-Lack of action-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2023_CEN23LA213.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 ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- 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…