ERA12CA581
2012-09-26 · Statesboro, Georgia, United States · None · 1 aircraft · Status: Completed
Airport TBR
Current FAA registration · N127AR
- Make / Model
- CESSNA 208B
- Year of manufacture
- 2004 · 8 years old at event
- Engine
- P&W PT6A SER (750 hp)
- Seats / Engines
- 12 seats · 1 engine
- Last airworthiness date
- 20040519
- ADS-B equipped
- Yes — Mode-S A06DC3
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s inadequate flare, which resulted in a hard landing.
Factual narrative
According to the flight instructor, the purpose of the flight was to complete recurrent training in the airplane. While on the downwind leg of the traffic pattern, the flight instructor configured the airplane for a simulated engine failure maneuver. The airplane was about a quarter mile from the runway on the base leg of the traffic pattern and the ground proximity warning system announced “500 feet.” As the pilot turned the airplane onto the final leg of the traffic pattern, the airplane overshot the centerline and it began to descend about 200 feet per minute. Then, about 150 feet above ground level, the pilot began to add power, but the airplane continued to descend and subsequently impacted the runway and bounced. The pilot recovered the airplane from the bounce, proceeded to takeoff and flew the airplane around the pattern. The occupants of the airplane noted that the left wing was bent and witness told them that the left main landing gear was bent. During the landing, the airplane veered off the runway and came to rest in a grassy area. During the accident sequence, the airplane incurred substantial damage to the left wing. The flight instructor reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. According to the flight instructor, the purpose of the flight was to complete recurrent training in the airplane. While on the downwind leg for a landing on runway 5, the flight instructor configured the airplane for a simulated engine failure maneuver. The pilot said he told the instructor that the airplane was too high for a landing on runway 5, so they agreed that he would land on runway 32.The pilot said that as he turned the airplane onto the final leg for runway 32, the airplane overshot the centerline and it began to descend about 200 feet per minute. About 150 feet above ground level, the pilot added power, but the airplane continued to descend and the left main gear and left wing tip impacted the runway and the airplane bounced. The pilot added full power and executed a go-around. The pilot said that during the go-around he noticed that the left outboard wing was bent and an observer in the back of the airplane reported that the left main landing gear was bent. The pilot said he flew the airplane around the pattern, and after the airplane landed, he noted it was difficult to steer the airplane and the airplane veered off the runway and came to rest in a grassy area. During the hard landing, the airplane sustained substantial damage to the left wing. The flight instructor reported 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-Landing flare-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2012_ERA12CA581.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 (engine failure, go-around). All research papers
- 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…
- 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…
- Semantic Scholar 2022 · Article (Journal of Safety Research) Go-around accidents and general aviation safety.
INTRODUCTION Changes in General Aviation (GA) accident rates, specifically in the go-around phase, are examined by comparing the number of accidents, the proportion of fatal accidents, and the proport…
- Semantic Scholar 2021 · Article (Aerospace) Classification and Analysis of Go-Arounds in Commercial Aviation Using ADS-B Data
Go-arounds are a necessary aspect of commercial aviation and are conducted after a landing attempt has been aborted. It is necessary to conduct go-arounds in the safest possible manner, as go-arounds …
- NASA NTRS 2021 · Accepted Manuscript (Version with final changes) Go-Around Criteria Refinement for Transport Category Aircraft
Presently, airline pilots are trained to go around if, when lower than 500 ft above the ground, they are outside of a handful of parameters such as airspeed, position, and rate of descent.