NTSB CAROL · Event
Event ERA25LA350
Registry · N580JA
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-181
Year of manufacture
2022 · 3 years old at event
Engine
LYCOMING IO-360-B4A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20220912
ADS-B equipped
Yes — Mode-S A776B1
Registrant of record
HOT WINGS AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On September 17, 2025 at 1000 eastern daylight time, a Piper PA-28-181 100i, N580JA, was substantially damaged when it was involved in an accident near Astatula, Florida. The student pilot sustained minor injuries. The airplane was operated as a 14 Code of Federal Regulations Part 91 instructional flight. The student pilot was performing three solo, full-stop/taxi-back landings. During her third landing approach, she executed a go-around due to traffic on the runway and departed the traffic pattern due to too much congestion. During the climb, she engaged the autopilot and set it for a climb, then switched fuel tanks. Once she was done switching fuel tanks, she saw that the airplane’s airspeed and engine’s rpm was increasing as the airplane descended. She disconnected the autopilot, reduced engine power, and leveled the airplane’s nose to stop the descent. A few seconds later, the airplane began to pitch down and descend again. She applied maximum back pressure on the controls to attempt to bring the nose back up, but the airplane remained in a descent. Upon realizing she was unable to arrest the descent, she located a dirt road and attempted to land. During the landing, the right wing struck a power pole, and a fence, resulting in substantial damage to the right and left wings; the right wing was partially impact-separated mid span and the left wingtip was crushed. Postaccident examination of the airplane revealed the stabilator trim tab was deflected to the full nose down position with the position of the flight control surface being consistent with the position of the indicator in the cockpit. The pilot stated that throughout the accident sequence, she did not manipulate the stabilator trim controls. The wreckage was retained for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_ERA25LA350.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 (go-around, autopilot). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2025 · arXiv preprint
ROSflight 2.0: Lean ROS 2-Based Autopilot for Unmanned Aerial Vehicles
ROSflight is a lean, open-source autopilot ecosystem for unmanned aerial vehicles (UAVs). Designed by researchers for researchers, it is built to lower the barrier to entry to UAV research and acceler…
- arXiv 2025 · arXiv preprint
ROSplane 2.0: A Fixed-Wing Autopilot for Research
Unmanned aerial vehicle (UAV) research requires the integration of cutting-edge technology into existing autopilot frameworks.
- 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 2024 · arXiv preprint
A Data-Driven Autopilot for Fixed-Wing Aircraft Based on Model Predictive Control
Autopilots for fixed-wing aircraft are typically designed based on linearized aerodynamic models consisting of stability and control derivatives obtained from wind-tunnel testing.
- arXiv 2022 · arXiv preprint
Experimental Flight Testing of a Fault-Tolerant Adaptive Autopilot for Fixed-Wing Aircraft
This paper presents an adaptive autopilot for fixed-wing aircraft and compares its performance with a fixed-gain autopilot.
Browse the full corpus — academia portal ↗