ERA14CA025
2013-10-26 · Tylertown, Mississippi, United States · None · 1 aircraft · Status: Completed
Airport T36
Current FAA registration · N812PT
- Make / Model
- MOONEY AIRPLANE CO INC M20TN
- Year of manufacture
- 2007 · 6 years old at event
- Engine
- CONT MOTOR TSIO-550-G (280 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20071004
- ADS-B equipped
- Yes — Mode-S AB1221
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's misjudgment of speed and distance on final approach resulting in touchdown prior to the runway, a runway excursion down the right side of the runway, and a collision with an embankment.
Factual narrative
According to the pilot, while on short final the airplane was "lower and slower" than anticipated. The pilot added engine power; however, the stall horn sounded and the airplane impacted the ground prior to the paved portion of the runway. The airplane bounced, traveled down the right side of the runway, collided with an embankment, and came to rest upright. Examination of the airplane by a Federal Aviation Administration inspector revealed that the empennage of the airplane sustained substantial damage. The pilot reported no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. According to the pilot, while on short final the airplane was "lower and slower" than anticipated. The pilot added engine power; however, the stall horn sounded and the airplane impacted the ground prior to the paved portion of the runway. The airplane bounced, traveled down the right side of the runway, collided with an embankment, and came to rest upright. Examination of the airplane by a Federal Aviation Administration inspector revealed that the empennage of the airplane sustained substantial damage. The pilot reported no preaccident 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-Descent/approach/glide path-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Personnel issues-Action/decision-Action-Lack of action-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2013_ERA14CA025.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 (stall, runway excursion). All research papers
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- SKYbrary (Eurocontrol) 2024 · SKYbrary article Runway Excursion — SKYbrary Knowledge Base
SKYbrary runway excursion review — RE-OE (overruns) + RE-LO (lateral). Risk drivers: long landing, high approach speed, contaminated surface, tailwind, mis-set autobrakes.
- 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
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- 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…