GAA18CA141
2018-02-23 · Show Low, Arizona, United States · None · 1 aircraft · Status: Completed
Airport SOW
Current FAA registration · N5147N
- Make / Model
- CESSNA 172M
- Seats / Engines
- 4 seats · 1 engine
- ADS-B equipped
- Yes — Mode-S A673A5
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor’s failure to maintain directional control during the landing roll in gusting crosswind and tailwind conditions.
Factual narrative
The flight instructor reported that, during approach in a gusting crosswind, he took the flight controls from the student pilot at about 500-700 ft. above ground level. He added that, during the landing roll while decelerating, a wind gust lifted up the back of the airplane "from the rear right to the front left forcing the front wheel onto the ground and lifting the plane onto the left main" landing gear. He applied full left rudder and right aileron to correct, but when it did not improve the situation he "relaxed the controls slightly back towards neutral". Subsequently, the airplane exited the runway to the right and came to rest inverted. The airplane sustained substantial damage to both wings, fuselage, and empennage. The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. A review of recorded data from the automated weather observation station located on the airport reported that, at the time of the accident, the wind was from 210° at 26 knots, gusting 32 knots. The airplane landed on runway 06. The flight instructor reported that, during approach in a gusting crosswind, he took the flight controls from the student pilot about 500 to 700 ft above ground level. He added that, during the landing roll while decelerating, a wind gust lifted the back of the airplane "from the rear right to the front left, forcing the front wheel onto the ground and lifting the plane onto the left main" landing gear. He applied full left rudder and right aileron to correct, but when it did not improve the situation, he "relaxed the controls slightly back towards neutral." Subsequently, the airplane exited the runway to the right and came to rest inverted. The airplane sustained substantial damage to both wings and the fuselage and empennage. The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The automated weather observation station located on the airport reported that, at the time of the accident, the wind was from 210° at 26 knots, gusting to 32 knots. The airplane landed on runway 06. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Instructor/check pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Effect on operation
- — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Effect on operation
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA18CA141.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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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.