NTSB CAROL · Event
Event ERA13LA099
Registry · N4340G
FAA Aircraft Registry record.
Make / Model
PIPER PA-28RT-201T
Year of manufacture
1984 · 28 years old at event
Engine
CONT MOTOR TSIO-360 SER (225 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19840130
ADS-B equipped
Yes — Mode-S A53459
Registrant of record
HAYNIE AIRLINE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper landing flare after a loss of engine power shortly after takeoff, which resulted in a hard landing. The reason for the loss of engine power could not be determined based on the available information.
Factual narrative
On December 23, 2012, about 1315 eastern standard time, a Piper PA28RT-201T, N4340G, was substantially damaged during a forced landing following a total loss of engine power on takeoff at Boca Raton Airport (BCT), Boca Raton, Florida. The private pilot and passenger were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight, which was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. The pilot stated that a pre-takeoff engine run-up revealed no anomalies, and he initiated a takeoff from runway 05. Shortly after rotation, he raised the airplane's landing gear. At an altitude about 100 feet above ground level, the engine suddenly "stopped without sputtering," and the airplane began to experience an aerodynamic stall. The pilot pitched the airplane's nose down, and subsequently attempted to flare the airplane for landing, and the airplane touched down on all three landing gear. The left main and nose landing gear collapsed, and the airplane slid off the left side of the runway, resulting in substantial damage to both wings. No examination of the engine or fuel system was conducted following the accident, and the reason for the loss of engine power could not be determined. The pilot held a private pilot certificate with ratings for airplane single-engine land and instrument airplane. The pilot reported 4,100 total flight hours of flight experience, of which 3,900 hours were in the accident make and model. His most recent FAA third-class medical certificate was issued in May 2011. The airplane was manufactured in 1984 and was equipped with a Continental Motors TSIO-360 series, 201 hp, turbocharged reciprocating engine. Its most recent annual inspection was completed on January 15, 2012. The engine had accumulated about 100 hours since its most recent overhaul. The airplane had accumulated 4,100 total hours in service at the time of the accident. The 1253 weather observation at Pompano Beach Airpark (PMP), Pompano Beach, Florida, located about 8 nautical miles south of the accident site, included wind from 110 degrees at 9 knots, 10 statute miles visibility, clear skies, temperature 21 degrees C, dew point 11 degrees C, and an altimeter setting of 30.21 inches of mercury. The pilot stated that a pretakeoff engine run-up revealed no anomalies and that he then initiated a takeoff. Shortly after rotation, the pilot selected the landing gear handle to the "up" position. When the airplane reached an altitude of about 100 ft above ground level, the engine suddenly "stopped without sputtering," and the airplane entered an aerodynamic stall. The pilot pitched the airplane's nose down and subsequently attempted to flare the airplane for landing; the airplane subsequently touched down on all three landing gear, which were in transition. The left main and nose landing gears collapsed, and the airplane slid off the left side of the runway, which resulted in substantial damage to both wings. Neither the engine nor the fuel system were examined following the accident, and the reason for the loss of engine power could not be determined. 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
- C Personnel issues-Action/decision-Action-Incorrect action performance-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_2012_ERA13LA099.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 (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗