ERA14CA023
2013-10-27 · Wauchula, Florida, United States · None · 1 aircraft · Status: Completed
Airport CHN
Current FAA registration · N725AS
- Make / Model
- CESSNA 182Q
- Year of manufacture
- 1978 · 35 years old at event
- Engine
- CONT MOTOR O-470 SERIES (230 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19781019
- ADS-B equipped
- Yes — Mode-S A9B630
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper landing flare which resulted in a hard landing.
Factual narrative
According to the pilot, after completing three takeoffs and landings at his destination airport he performed a simulated engine failure. Upon entered the landing phase of the flight he was excessively high above the runway surface. "Fixated" on completing the landing, the pilot flared the airplane too high which resulted in a hard landing and collapse of the nose gear, damage to the propeller, and damage to the aircraft structure. A post-accident examination of the wreckage revealed substantial damage to the firewall. The pilot reported no pre-accident mechanical malfunctions or anomalies that could have precluded normal operation. The pilot stated he could have prevented the accident by performing a go around. According to the pilot, after completing three takeoffs and landings at his destination airport he performed a simulated engine failure. Upon entered the landing phase of the flight he was excessively high above the runway surface. "Fixated" on completing the landing, the pilot flared the airplane too high which resulted in a hard landing and collapse of the nose gear, damage to the propeller, and damage to the aircraft structure. A post-accident examination of the wreckage revealed substantial damage to the firewall. The pilot reported no pre-accident mechanical malfunctions or anomalies that could have precluded normal operation. The pilot stated he could have prevented the accident by performing a go around. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation - C
Verbatim from NTSB's published report. Source file
NTSB_2013_ERA14CA023.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 ↗
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- Pilots of America Community ↗
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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…