NTSB CAROL · Event
Event FTW02LA029
Registry · N96LS
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR22T
Year of manufacture
2019
Engine
CONT MOTOR TSIO-550-K (315 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
20190710
ADS-B equipped
Yes — Mode-S AD5AD8
Registrant of record
STABLER RANDALL
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to perform a preflight inspection, which resulted in a loss of total engine power due to oil starvation. A contributing factor was the lack of suitable training for the forced landing.
Factual narrative
On November 3, 2001, approximately 1500 central standard time, a Landoll Vans RV 3-A single-engine homebuilt experimental airplane, N96LS, was substantially damaged when it struck trees and terrain during a forced landing following a loss of engine power during takeoff from the Denton Municipal Airport, Denton, Texas. The airplane was owned by N96LS Club LTD of Wilmington, Delaware. The commercial pilot, operator and sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight was originating at the time of the accident. The pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that he had spent most of the day waxing his airplane and decided to fly it once around the pattern. The engine start-up, taxi, and engine run-up "indications were normal." During climb out after takeoff from runway 17, he had turned crosswind and had climbed to 600 feet when the engine lost power. The pilot turned downwind, switched fuel tanks, and attempted, unsuccessfully, to restart the engine. The pilot determined that he could not make it back to the runway and initiated a forced landing, without flaps, to a field. During the approach, the airplane impacted small trees and vegetation. Subsequently, the airplane impacted the ground and came to rest upright. An examination of the airplane, by the FAA inspector who responded to the accident site, revealed that both wing fuel tanks were full of fuel. Both the left and right wings sustained substantial damage, and the left main landing gear was found separated. The engine was found "seized," and it contained no oil. No evidence of an oil leak was found. The mechanic, who had been servicing the airplane, reported to the FAA inspector that he had drained the oil from the airplane's engine, left the airplane unattended, and had not replenished the oil before the accident flight. The pilot had spent most of the day waxing his airplane and decided to fly it once around the pattern. The engine start-up, taxi, and engine run-up "indications were normal." While climbing out at 600 feet agl, the engine lost power. The pilot attempted, unsuccessfully, to restart the engine. During a forced landing to a field, the airplane impacted small trees and vegetation. Examination of the engine revealed it was "seized" and contained no oil. No evidence of an oil leak was found. The mechanic, who had been servicing the airplane, reported to the FAA inspector that he had drained the oil from the airplane's engine, left the airplane unattended, and had not replenished the oil prior to the accident flight. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_FTW02LA029.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 ↗