NTSB CAROL · Event
Event GAA19CA199
Registry · N925SF
FAA Aircraft Registry record.
Make / Model
BEECH G36
Year of manufacture
2009 · 10 years old at event
Engine
CONT MOTOR IO-550-B (300 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
20090921
ADS-B equipped
Yes — Mode-S ACD253
Registrant of record
PEIFER CHARLES R
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control and runway heading during landing, which resulted in a runway excursion and the nose landing gear collapsing.
Factual narrative
The pilot reported that, during approach to runway 16 on the private airstrip, the electronic primary flight display reported the wind from the south at 16 knots. He added that, during landing, the airplane touched down, but the airplane quickly veered to the left. He added power to correct and "the addition of power was enough to lift the airplane slightly, but not to take off again, and so after [he] floated a short distance, [the airplane] landed again off the side of the runway." The nose landing gear collapsed in the dirt. The airplane sustained substantial damage to the right wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot reported that, during approach to a private airstrip, the electronic primary flight display reported that the wind was from the south at 16 knots. He added that, upon touchdown, the airplane quickly veered left. He added power to correct, and "the addition of power was enough to lift the airplane slightly, but not to take off again, and so after [the airplane] floated a short distance, [it] landed again off the side of the runway." The nose landing gear collapsed in the dirt. The airplane sustained substantial damage to the right wing. The pilot reported that there were no preaccident mechanical failures or malfunctions 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Heading/course-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Physical environment-Runway/land/takeoff/taxi surface-Soft surface-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA199.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 (runway excursion). 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
This paper presents an Internet of things 36-rotor unmanned aerial vehicle suitable for radiological surveying of buildings and facilities.
- 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.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Runway Excursion — SKYbrary Knowledge Base
SKYbrary runway excursion review — RE-OE (overruns) + RE-LO (lateral). Risk drivers: long landing, high approach speed, contaminated surface, tailwind, mis-set autobrakes.
Browse the full corpus — academia portal ↗