ERA14CA375
2014-08-06 · Valkaria, Florida, United States · Minor · 1 aircraft · Status: Completed
Airport X59
Current FAA registration · N9400E
- Make / Model
- CESSNA 172N
- Year of manufacture
- 1979 · 35 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19790202
- ADS-B equipped
- Yes — Mode-S AD0F85
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's misjudgment of speed and distance on final approach during a precautionary landing, resulting in a touchdown off the departure end of the runway and collision with terrain. A factor in the accident was a partial loss of engine power for reasons that could not be determined in post accident testing.
Factual narrative
According to the student pilot, she had just landed after a local instructional flight. Her instructor completed the solo endorsement in her logbook as they taxied back to the arrival end of the runway 28. The student pilot then taxied on to runway 28 for departure. She applied full throttle and the airplane lifted off the runway normally. At approximately 500 feet above ground level the engine began to run rough and dropped to 1900 RPMs. The student pilot immediately lowered the nose of the airplane to attain best glide speed and started a left hand turn to return to the airport. She attempted to land on runway 10. Approximately 20 seconds after the engine began running rough the pilot applied the carburetor heat and then reduced the throttle to idle. The student pilot did not attempt however to increase power after the application of carburetor heat and the throttle remained in the idle position for the remainder of the approach. The pilot then applied full flaps as the airplane was descending over midfield. The airplane overflew the runway and touched down in the grass immediately off the departure end of runway 10. The airplane subsequently struck a fence and nosed over. Post accident examination of the airplane and engine showed no evidence of mechanical failure or malfunction. The engine was started and operated with no signs of failure. A review of the carburetor icing probability chart shows the aircraft was operating in conditions that were not conductive to carburetor icing at the time of the accident. The pilot had 43 total flight hours. According to the student pilot, she had just landed after a local instructional flight. Her instructor completed the solo endorsement in her logbook as they taxied back to the arrival end of the runway 28. The student pilot then taxied on to runway 28 for departure. She applied full throttle and the airplane lifted off the runway normally. At approximately 500 feet above ground level the engine began to run rough and dropped to 1900 RPMs. The student pilot immediately lowered the nose of the airplane to attain best glide speed and started a left hand turn to return to the airport. She attempted to land on runway 10. Approximately 20 seconds after the engine began running rough the pilot applied the carburetor heat and then reduced the throttle to idle. The student pilot did not attempt however to increase power after the application of carburetor heat and the throttle remained in the idle position for the remainder of the approach. The pilot then applied full flaps as the airplane was descending over midfield. The airplane overflew the runway and touched down in the grass immediately off the departure end of runway 10. The airplane subsequently struck a fence and nosed over. Post accident examination of the airplane and engine showed no evidence of mechanical failure or malfunction. The engine was started and operated with no signs of failure. A review of the carburetor icing probability chart shows the aircraft was operating in conditions that were not conductive to carburetor icing at the time of the accident. The pilot had 43 total flight hours. 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-Airspeed-Incorrect use/operation - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Descent/approach/glide path-Incorrect use/operation - C
- F Not determined-Not determined-(general)-(general)-Unknown/Not determined - F
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Student/instructed pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2014_ERA14CA375.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 (icing). All research papers
- arXiv 2026 · arXiv preprint Enabling Beyond-Visual-Line-of-Sight Drones Operation over Open RAN 5G Networks with Slicing
Among the foretold claims of the transition from 5G to 6G, Beyond-Visual-Line-of-Sight (BVLoS) drone operation has emerged as a prominent Internet-of-Robots enabler.
- NASA NTRS 2026 · Contractor Report (CR) Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- NASA NTRS 2025 · Presentation NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- arXiv 2024 · arXiv preprint An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…