NTSB CAROL · Event
Event GAA19CA102
Registry · N636M
FAA Aircraft Registry record.
Make / Model
FLEET 1
Year of manufacture
1930 · 88 years old at event
Engine
KINNER K5 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20210204
ADS-B equipped
Yes — Mode-S A85519
Registrant of record
TSI HOLDCO INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain the proper airspeed during landing, which resulted in the airplane landing too fast and too far down the runway to safely stop it.
Factual narrative
The pilot reported that he was flying a recently purchased airplane. During initial climb, the front right-side cockpit door opened. He decided that the condition was unsafe and entered a left downwind to land. The approach end of the runway had rising terrain, and the airplane was too high and too fast. About 200ft AGL he decided to abort the landing, but the engine sputtered. Still too fast, the airplane landed about 1,500ft down the 5,132ft runway, and he immediately applied the brakes. However, the airplane overran the runway and collided with a fence. The airplane sustained substantial damage to the left wing and the elevator. The pilot reported that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot reported that he was flying a recently purchased airplane. During initial climb, the front right cockpit door opened. He decided that the condition was unsafe and entered a left downwind to land. The approach end of the runway had rising terrain, and the airplane was too high and fast. About 200 ft above ground level, he decided to abort the landing, but the engine sputtered, and he continued the landing. The airplane overran the runway and collided with a fence. The airplane sustained substantial damage to the left wing and the elevator. The pilot reported that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- — Environmental issues-Physical environment-Object/animal/substance-Fence/fence post-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA19CA102.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 2022 · arXiv preprint
Zero Touch Coordinated UAV Network Formation for 360° Views of a Moving Ground Target in Remote VR Applications
Unmanned aerial vehicles (UAVs) with on-board cameras are widely used for remote surveillance and video capturing applications.
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA)
Internet of Things 36-rotor Multicopter for Ionizing Radiation Surveying
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- NASA NTRS 2019 · Other - NACA Research Memorandum
Ditching Tests of Two Models of the Army B-36 Airplane
The ditching characteristics of the Army B-36 airplane were determined by testing 1/20- and 1/30-scale dynamic models in calm water in Langley tank no. 2 and at the outdoor catapult.
- NASA NTRS 2019 · Other
Differential Pressures on a Pitot-venturi and a Pitot-static Nozzle over 360 Degrees Pitch and Yaw
Measurements of the differential pressures on two navy air-speed nozzles, consisting of a Zahm type Pitot-Venturi tube and a SQ-16 two-pronged Pitot-static tube, in a tunnel air stream of fixed speed …
- NASA NTRS 2019 · Technical Memorandum (TM)
Flutter clearance of the Schweizer 1-36 deep-stall sailplane
A Schweizer 1-36 sailplane was modified for a controlled, deep-stall flight program. This modification allowed the horizontal stabilizer to pivot as much as 70 deg leading edge down.
- NASA NTRS 2026 · Technical Memorandum (TM)
Assessing National Airspace System Impact of the Hybrid Electric Turboprop Commercial Freighter
The Hybrid Electric Turboprop Commercial Freighter (HETCOF) is a large turboprop aircraft using hybrid electric propulsion designed to reduce cost and emissions for narrowbody cargo operations capable…
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