GAA17CA081
2016-11-17 · Destin, Florida, United States · None · 1 aircraft · Status: Completed
Airport DTS
Current FAA registration · N9358L
- Make / Model
- CESSNA 172P
- Year of manufacture
- 1986 · 30 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19860117
- ADS-B equipped
- Yes — Mode-S ACFBB7
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot’s overcorrection with right rudder, which resulted in a loss of directional control, and the flight instructor’s delayed remedial action.
Factual narrative
The student pilot reported that during the landing roll of a touch-and-go the airplane was off the centerline and he added right rudder, but he "overcompensated". The flight instructor reported that the airplane drifted to the right and was about to exit the runway, so he pushed in the throttle, applied left rudder, and pulled back on the yoke to initiate a climb. The student pilot reported that as the airplane became airborne they heard a "slight bang" and thought the landing gear had struck a runway light. The flight instructor further reported that they conducted a full-stop landing to examine the landing gear, but there was no damage noted. During a postflight inspection at their home airport, it was revealed that the left horizontal stabilizer had sustained substantial damage. The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The student pilot reported that during the landing roll of a touch-and-go the airplane was off the centerline and he added right rudder, but he "overcompensated". The flight instructor reported that the airplane drifted to the right and was about to exit the runway, so he pushed in the throttle, applied left rudder, and pulled back on the yoke to initiate a climb. The student pilot reported that as the airplane became airborne they heard a "slight bang" and thought the landing gear had struck a runway light. The flight instructor further reported that they conducted a full-stop landing to examine the landing gear, but there was no damage noted. During a postflight inspection at their home airport, it was revealed that the left horizontal stabilizer had sustained substantial damage. The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
- C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
- C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Student/instructed pilot - C
- — Environmental issues-Physical environment-Object/animal/substance-Runway/taxi/approach light-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2016_GAA17CA081.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.
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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.