NTSB CAROL · Event
Event LAX00LA032
Registry · N183DA
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR20
Year of manufacture
2003
Engine
CONT MOTOR GTSIO-520-C (340 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20030918
ADS-B equipped
Yes — Mode-S A14C1D
Registrant of record
HULLMANN JOHN
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control of the airplane during the touch-and-go takeoff.
Factual narrative
On November 11, 1999, at 1247 hours Pacific standard time, a Diamond Aircraft Industries (Katana) DA 20-A1, N183DA, veered off runway 01R and struck a windsock pole between the runway and taxiway at Buchanan Field, Concord, California. The airplane, owned and operated by Concord Flight International under 14 CFR Part 91 as an instructional flight, sustained substantial damage. The student pilot, the sole occupant, was not injured. Visual meteorological conditions existed for the local area instructional flight and no flight plan was filed. The student pilot stated that he had gone up to practice touch-and-go takeoffs and landings. On the first touch-and-go landing he noted that he was too high and initiated a go-around. The next two touch-and-go takeoffs and landings were executed with no discrepancies. He stated that on short final for the third one, the airplane was blown slightly off centerline. He returned the airplane to centerline and stated that there were no further discrepancies with the approach. The airplane landed on centerline just past the runway numbers, and he "got rid of a notch of flaps, and pushed the carburetor heat in." The pilot stated that he advanced the throttle and the airplane "snapped" to the left. He applied right rudder, which stopped the turn to the left, but did not return the airplane to the runway. The airplane continued off of the runway before he reduced the throttle. The pilot stated that he did not apply brakes at any time and that there were no perceived anomalies with the flight control system. The left wing of the airplane struck the windsock pole and the airplane came to rest on a westerly heading from the direction of travel. The right main landing gear was ripped off and the engine was still running. The pilot shut the airplane down and notified the tower that he was all right via a handheld radio. According to a Federal Aviation Administration inspector, there were no signs of a skid mark present on the runway, grass, gravel, asphalt, or dirt areas where the accident occurred. He conducted an inspection of the airplane's rudder, braking system and wheels and observed no abnormalities. The aviation surface weather report for the airport was reporting winds from 360 degrees at 8 knots. The student pilot was practicing touch-and-go takeoffs and landings. On the third approach he noted the airplane was blown slightly off centerline, and he corrected back to centerline. The airplane landed on the centerline just past the runway numbers. He adjusted the flaps up one notch and pushed the carburetor heat in. As he advanced the throttle, the airplane veered to the left off of the runway. The airplane struck the windsock pole located between the runway and a taxiway. The area where the accident occurred was observed to have no skid marks or tire tracks. The airplane rudder braking system and wheels were inspected with no abnormalities noted. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_LAX00LA032.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, go-around). 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 · 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.
- 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…
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