GAA19CA130
2019-02-04 · Hanover, Virginia, United States · None · 1 aircraft · Status: Completed
Airport OFP
Current FAA registration · N9525V
- Make / Model
- CESSNA 172R
- Year of manufacture
- 1998 · 21 years old at event
- Engine
- LYCOMING I0360 SER A&C (200 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19980119
- ADS-B equipped
- Yes — Mode-S AD3F30
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's improper decision to release the seat latch to adjust the seat position during taxi, which resulted in his inability to reach the rudder or brake pedals and a subsequent loss of directional control and impact with a ditch and fence.
Factual narrative
The solo student pilot reported that while taxiing to the runway for departure, he attempted to adjust the seat to get a "better view". When he released the seat latch, the seat moved aft, and he was unable to reach the rudder pedals or brake pedals with his feet. He added that he was unable to lean forward because his seat belt was secured. Subsequently, the airplane veered left, he pulled the engine throttle to idle, but the airplane exited the taxiway into a ditch and struck a wire fence. The airplane sustained substantial damage to the left wing and right horizontal stabilizer. The student pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The solo student pilot reported that, while taxiing to the runway for departure, he attempted to adjust the seat to get a "better view." When he released the seat latch, the seat moved aft, and he was unable to reach the rudder pedals or brake pedals with his feet. He added that he was unable to lean forward because his seat belt was secured. Subsequently, the airplane veered left, and he pulled the engine throttle to idle, but the airplane exited the taxiway into a ditch and struck a wire fence. The airplane sustained substantial damage to the left wing and right horizontal stabilizer. The student 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
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft structures-Fuselage-Seat/cargo attach fitting-Incorrect use/operation - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Student/instructed pilot - C
- — Environmental issues-Physical environment-Object/animal/substance-Fence/fence post-Contributed to outcome
- — Environmental issues-Physical environment-Terrain-Sloped/uneven terrain-Contributed to outcome
- — Environmental issues-Task environment-Physical workspace-Access to equipment/controls-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA130.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
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- Pilots of America Community ↗
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- 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.