NTSB CAROL · Event
Event GAA18CA437
Registry · N3224D
FAA Aircraft Registry record.
Make / Model
CESSNA 180
Year of manufacture
1954 · 64 years old at event
Engine
AMA/EXPR UNKNOWN ENG
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19541220
ADS-B equipped
Yes — Mode-S A378A6
Registrant of record
E W AIRCRAFT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during landing.
Factual narrative
The pilot of the tailwheel equipped airplane reported that, after a wheel landing, the tail wheel touched down on the ground and started a "violent shaking." He pushed forward on the control yoke to raise the tail, increase throttle and subsequently let the tail touched down on the runway again. The tailwheel continued to shake, and the airplane began to veer left but the pilot corrected with opposite rudder. Shortly after the airplane regained runway heading, the airplane veered right, exited the runway to the right and ground looped. The airplane sustained substantial damage to the left wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot added that, during landing, the wind was from 010º at 4 knots. The automated weather observation station located on the airport reported that, about the 15 minutes before the accident, the wind was from 160° at 4 knots. The airplane landed on runway 03. The pilot did not submit the National Transportation Safety Board Pilot/Operator Aircraft Accident/Incident Report Form 6120.1. The pilot of the tailwheel-equipped airplane reported that, after a wheel landing, the tailwheel touched down, and it then started shaking violently. In an attempt to stop the shaking, he pushed forward on the control yoke to no avail. He then tried adding power, raised the tail, and let the tailwheel touch down again; however, the tailwheel continued to shake, and the airplane began to veer left, and he corrected by applying right rudder. Shortly after the airplane regained the runway heading, it suddenly veered right, exited the runway to the right, and ground looped. The airplane sustained substantial damage to the left wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot added that, during landing, the wind was from 010º at 4 knots. The airport's automated weather observation station reported that, about the 15 minutes before the accident, the wind was from 160° at 4 knots. The pilot landed the airplane on runway 03. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA18CA437.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. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2026 · arXiv preprint
A Miniaturized Broadband 1-Bit Coding Reconfigurable Intelligent Surface for NLOS UE Localization and Uplink Communication
In this paper, a broadband 1-bit coding metasurface-based reconfigurable intelligent surface (RIS) is presented. The unit cell of the metasurface consists of a wide dipole modified with interdigital c…
- arXiv 2024 · arXiv preprint
Distilling Tiny and Ultra-fast Deep Neural Networks for Autonomous Navigation on Nano-UAVs
Nano-sized unmanned aerial vehicles (UAVs) are ideal candidates for flying Internet-of-Things smart sensors to collect information in narrow spaces.
- arXiv 2024 · arXiv preprint
A flexured-gimbal 3-axis force-torque sensor reveals minimal cross-axis coupling in an insect-sized flapping-wing robot
The mechanical complexity of flapping wings, their unsteady aerodynamic flow, and challenge of making measurements at the scale of a sub-gram flapping-wing flying insect robot (FIR) make its behavior …
- Embry-Riddle Scholarly Commons 2024 · Conference paper
Integrated Propulsion and Control of Rotorcraft
RESEARCH OBJECTIVE OVERVIEW The Eagle Flight Research Center (EFRC) at Embry-Riddle Aeronautical University (ERAU) is investigating the handling qualities of failure modes of multi-rotors employing di…
- NASA NTRS 2023 · Presentation
Subsonic Single Aft Engine (SUSAN) Flight Deck Experiment: Throttle and Engine Display Concepts
NASA is developing a new hybrid-electric aircraft concept called the SUbsonic Single Aft eNgine (SUSAN) Electrofan. The SUSAN airplane is being designed as a 180-passenger commercial regional jet and …
- Embry-Riddle Scholarly Commons 2023 · Conference paper
The Value of Strong Partnerships to Build a Successful Aviation Maintenance Career Pathway Program for Transitioning Military Service Members
The aerospace industry is competing with other industries for a qualified workforce, and many of those competing industries are investing heavily in creating workforce development pipelines.
Browse the full corpus — academia portal ↗