GAA19CA326
2019-06-08 · ORLANDO, Florida, United States · None · 1 aircraft · Status: Completed
Airport ISM
Current FAA registration · N1589D
- Make / Model
- CESSNA 172R
- Year of manufacture
- 2005 · 14 years old at event
- Engine
- LYCOMING IO-360-L2A (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20051102
- ADS-B equipped
- Yes — Mode-S A0EB7E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's excessive rudder application during takeoff and the flight instructor's delayed remedial action, which resulted in a loss of directional control, a runway excursion, and subsequent substantial damage.
Factual narrative
The flight instructor reported that, while the student pilot was practicing soft field takeoffs, the student added full power and maintained back pressure. He told the student to add right rudder, but the airplane veered left. The instructor told the student to add right rudder again, then the student abruptly added right rudder. The airplane veered to the right, the instructor attempted to correct, but the airplane exited the runway to the right, and the right wing and right horizontal stabilizer impacted the ground. The airplane sustained substantial damage to the right wing and right horizontal stabilizer. The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The flight instructor reported that, while the student pilot was practicing soft-field takeoffs, the student added full power and maintained back pressure. He told the student to add right rudder, but the airplane veered left. The instructor told the student to add right rudder again, then the student abruptly added right rudder. The airplane veered right, the instructor attempted to correct, but the airplane exited the runway to the right, and the right wing and right horizontal stabilizer impacted the ground. The airplane sustained substantial damage to the right wing and right horizontal stabilizer. The instructor reported that there were no preaccident mechanical failures or malfunctions 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-Directional control-Not attained/maintained - C
- C Aircraft-Aircraft systems-Flight control system-Rudder control system-Incorrect use/operation - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
- C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
- C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Student/instructed pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA326.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 ↗
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Related research
Matched on aircraft type or causal vocabulary (icing, runway excursion). All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- 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…