FTW99LA043
1998-12-03 · SPRINGDALE, Arkansas, United States · None · 1 aircraft · Status: Completed
Airport ASG
Current FAA registration · N1774C
- Make / Model
- CESSNA 180
- Year of manufacture
- 1953 · 45 years old at event
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19540326
- ADS-B equipped
- Yes — Mode-S A13615
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper recovery from a bounced landing resulting in a ground loop. A factor was the pilot's improper landing flare.
Factual narrative
On December 3, 1998, at 1658 central standard time, a Cessna 180, tailwheel equipped airplane, N1774C, was substantially damaged following a loss of control while landing at Springdale, Arkansas. The private pilot and his 2 passengers were not injured. The airplane was owned and operated by a private individual under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the personal cross for which no flight plan was filed. The 194 nautical mile cross country flight originated from the Thompson-Robbins Airport, near Helena, Arkansas, at 1515. According to personnel at the control tower, the aircraft "ground looped after the pilot lost directional control of the airplane" while on the landing roll on runway 18. In a written statement, the pilot reported that "everything seemed normal during the approach until the airplane touched down in a full stall configuration with 20 degrees of flaps." The pilot added that "the airplane bounced on touchdown and after it settled back on the runway, the airplane began a sharp left turn toward the edge of the runway." Subsequently, the right wing struck the ground and the airplane nosed over coming to rest in the inverted position on the east side of the runway. The winds at the time of the accident were reported from 190 degrees at 10 knots. Examination of the airplane by personnel at the airport revealed that the left wing strut and the vertical stabilizer sustained structural damage. The FAA inspector confirmed the damage and examined the airplane's landing gear brakes and steering mechanism. No defects were found on either systems. The 77 hour private pilot earned his pilot certificate in October 1998, and had accumulated a total of 30 flight hours in this make and model airplane. The passengers were the pilot's wife and their infant child who was strapped to an automotive type child seat. The 1953 vintage airplane was equipped with shoulder harnesses for all occupants. The private pilot lost control of the tailwheel equipped airplane during the landing roll on runway 18. Personnel at the control tower reported that the aircraft ground looped after the pilot lost directional control of the airplane after the airplane bounced. The pilot stated that the airplane bounced on touchdown and after it settled back on the runway, the airplane began a sharp left turn toward the edge of the runway. Subsequently, the right wing struck the ground and the airplane nosed over coming to rest in the inverted position on the east side of the runway. The winds at the time of the accident were reported from 190 degrees at 10 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_FTW99LA043.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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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 …