NTSB CAROL · Event
Event GAA17CA232
Registry · N92873
FAA Aircraft Registry record.
Make / Model
CESSNA 172M
Year of manufacture
1973 · 44 years old at event
Engine
LYCOMING 0-360 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19730412
ADS-B equipped
Yes — Mode-S ACDF4B
Registrant of record
SONDAY TERRANCE P
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s delayed attempt to abort the takeoff with a tailwind, which resulted in a runway overrun.
Factual narrative
The pilot of the float-equipped airplane reported that prior to takeoff, the windsock showed "no significant wind" and the control tower "confirmed using a southerly traffic pattern". He added that during the takeoff on the waterway, the airplane initially accelerated as expected. He further added that "it became clear that the take-off run was not progressing as anticipated" and decided to abort the takeoff. He brought the power to idle and applied back pressure to the control yoke. The airplane slid onto the grass embankment at the end of the runway and came to rest on the adjacent taxiway. The airplane sustained substantial damage to the fuselage. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Weather observations, located on the airport, showed that from about 20 minutes before the accident to 60 minutes after the accident, the wind varied in direction from 360° to 050°, and the speed varied 4 to 11 knots, with a peak wind of 360° at 30 knots. The pilot departed waterway 17W. The pilot of the float-equipped airplane reported that, before takeoff, the windsock showed "no significant wind" and that the control tower "confirmed using a southerly traffic pattern." He added that, during the takeoff from the waterway, the airplane initially accelerated as expected. He further added that "it became clear that the take-off run was not progressing as anticipated" and that he decided to abort the takeoff. He brought the power to idle and applied back pressure to the control yoke. The airplane slid onto the grass embankment at the end of the runway and came to rest on the adjacent taxiway. The airplane sustained substantial damage to the fuselage. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Weather observations from the airport showed that, from about 20 minutes before the accident to 60 minutes after the accident, the wind varied in direction from 360° to 050°, and the speed varied from 4 to 11 knots, with a peak wind from 360° at 30 knots. The pilot departed waterway 17W. 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-Aircraft capability-Takeoff distance-Capability exceeded - C
- C Personnel issues-Action/decision-Action-Delayed action-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Sudden wind shift-Effect on operation
- — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2017_GAA17CA232.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.
- NASA NTRS 2019 · Conference Paper
Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM)
Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- Embry-Riddle Scholarly Commons 2023 · Conference paper
Validation of Training Satisfaction Survey
The Training Satisfaction Survey (TSS) was developed as part of a larger project to examine the features of Virtual Reality software and supporting devices as a training program on visual illusions an…
- Semantic Scholar 2021 · Article (Data in Brief)
Cockpit voice recorder transcript data: Capturing safety voice and safety listening during historic aviation accidents
Cockpit Voice Recorder (CVR) transcripts capture audio data within cockpit environments. This aids the investigation of causal factors contributing to aviation accidents by revealing communication and…
- Semantic Scholar 2021 · Article (Safety Science)
Safety voice and safety listening during aviation accidents: Cockpit voice recordings reveal that speaking-up to power is not enough
Abstract Safety voice is theorised as an important factor for mitigating accidents, but behavioural research during actual hazards has been scant.
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Can Backward-Chained, Ab-Initio Pilot Training Decrease Time to First Solo?
Flight simulation has made progressively significant inroads into pilot training at all levels of a pilot’s career – typically starting with training for the Instrument rating in light aircraft and co…
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