ATL00LA001
1999-10-22 · MORGANTON, North Carolina, United States · None · 1 aircraft · Status: Completed
Airport MRN
N3255H has since been reassigned. It is now registered to a different aircraft (ROBINSON HELICOPTER R44 II, built 2007), which was not involved in this event.
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for a tailwind which resulted in the loss of control.
Factual narrative
On October 22, 1999, at 1900 eastern daylight time, a Cessna 305C, N3255H, nosed over on landing at Morganton Airport in Morganton, North Carolina. The personal flight was operated by the private pilot under the provisions of Title 14 CFR Part 91 and visual flight rules. Visual meteorological conditions prevailed at the time of the accident and no flight plan was filed. The airplane was substantially damaged and the pilot was not injured. The flight departed Lincolnton, North Carolina, at 1730. According to the FAA, the wind condition at Morganton Airport at the time of the accident was reported as 10 knots gusting to 15 knots from a direction of 300 degrees to 320 degrees. Of the two runways available, runway 21 and runway 3, the pilot decided on runway 21 because he believed the winds were favoring that runway. The pilot believed he was landing on runway 21, when in fact, he landed on runway 3. According to the pilot, he landed with 30 degrees of flaps while applying right rudder to correct for wind drift. The stall warning horn sounded as the main gear touched down. As the tailwheel settled, the tail of the airplane started drifting to the right edge of the runway. He applied additional right rudder to straighten the airplane, but it had no effect. At this time, he realized he did not have enough rudder control to arrest the drift of the airplane. He applied additional power in an attempt to regain rudder effectiveness. The airplane straightened briefly but he decided to abort the landing and applied full power to go around. At that time, he lost directional control of the airplane and ground looped the airplane. The left wing struck the ground to the left of the runway. The airplane nosed over, slid, and came to rest on its back. The pilot exited the airplane uninjured. Examination of the wreckage revealed structural damage to the left wingtip, vertical stabilizer, rudder, and right wing strut. Additionally, the top surfaces of both wings were wrinkled. The engine and propeller assemblies were damaged and the engine was partially torn from the engine mounts. The engine was further damaged by fire that was contained to the engine compartment. No mechanical deficiencies with the airplane were reported by the pilot. The pilot believed the winds favored runway 21, and believed he was landing on runway 21, when in fact, he landed on runway 3. According to the pilot, he landed with 30 degrees of flaps while applying right rudder to correct for wind drift. The stall warning horn sounded as the main gear touched down. As the tailwheel settled, the tail of the airplane started drifting to the right edge of the runway. His further attempts to gain directional control of the airplane were ineffective. The airplane then ground looped and nosed over. Winds at the airport were reported to be from 330 degrees at 12 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_ATL00LA001.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (stall, loss of control). All research papers
- Semantic Scholar 2016 · Article (Interacción) Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
In Urban Air Mobility (UAM), maintaining a minimum separation between aircraft is a safety requirement, which becomes challenging amidst congested air traffic and off-nominal conditions, such as Loss …