NTSB CAROL · Event
Event MIA05CA099
Registry · N146SW
FAA Aircraft Registry record.
Make / Model
PIPER PA-32-301
Year of manufacture
1980 · 25 years old at event
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
7 seats · 1 engine
Last airworthiness date
20030523
ADS-B equipped
Yes — Mode-S A0BA9F
Registrant of record
FAIRWAY SYSTEMS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot-in-command failure to maintain directional control during takeoff after landing, which resulted in the airplane exiting the runway.
Factual narrative
On April 28, 2005 about 1430 eastern daylight time, a Piper PA-32-301, N146SW, registered to Fairway Systems LLC and operated by a private individual as a Title 14 CFR Part 91 personal flight, lost directional control of the aircraft while on a touch-and-go landing at Hernando County Airport, Brooksville, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The private-rated pilot and passenger received no injuries, and the aircraft incurred substantial damage. The flight originated from the same airport, earlier that day, about 1330. The pilot-in-command stated, she was practicing instrument approaches to runway 09 with a safety pilot. When the airplane approached an indicated altitude of about 700 feet, she removed the view-limiting device to transition from an instrument to a visual approach. Upon landing the pilot-in-command pushed the propeller lever forward and applied full engine power. The airplane veered off the left side of the runway onto grass terrain. The nose landing gear collapsed and the propeller struck the ground before coming to a full stop. A licensed FAA airframe and powerplant mechanic inspected the airplane after the accident and stated the steering actuation system was properly connected, the flight controls operated normally, and the brake system functioned properly. There were no discrepancies found with the systems. The pilot-in-command stated that she was practicing instrument approaches to runway 09 with a safety pilot. When the airplane approached an indicated altitude of about 700 feet, she removed the view-limiting device to transition from an instrument to a visual approach for the touch-and-go. Upon landing the pilot-in-command pushed the propeller lever forward and applied full engine power. The airplane veered off the left side of the runway onto grass terrain incurring substantial damage. An A&P mechanic inspected the airplane after the accident and found no discrepancies with the airplane's steering systems, the flight controls operated normally, and the brake system functioned properly. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_MIA05CA099.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 (icing). 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 · 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…
- 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…
- 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…
- 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…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗