GAA19CA424
2019-07-16 · Grand Canyon, Arizona, United States · None · 1 aircraft · Status: Completed
Airport GCN
Current FAA registration · N1079M
- Make / Model
- CESSNA 172L
- Year of manufacture
- 1971 · 48 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19710605
- ADS-B equipped
- Yes — Mode-S A02254
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain lateral control during landing in gusting wind conditions, which resulted in the left wing striking the ground.
Factual narrative
The pilot reported that, during approach to land, he corrected for a left crosswind. After crossing the threshold, he reduced power and as he was about to touch down, the airplane "rolled" to the left and the left wing struck the runway. The airplane immediately "righted itself" and he landed the airplane. He added that the runway strike caused a "minor misalignment" with the airplane. The airplane sustained substantial damage to the left wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The airport's automated weather observation station reported that, about 36 minutes before the accident, the wind was from 210° at 11 knots, gusting to 19 knots. The same automated station reported that, about 24 minutes after the accident, the wind was from 210° at 17 knots, gusting to 25 knots, with a peak wind reported 3 minutes after the accident from 220° at 27 knots. The pilot landed the airplane on runway 21. The pilot reported that, during approach to land, he corrected for a left crosswind. After crossing the threshold, he reduced power and as the airplane was about to touch down, it "rolled" left, and the left wing struck the runway. He added that the airplane immediately "righted itself" and that he then landed it. The airplane sustained substantial damage to the left wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The airport's automated weather observation station reported that, about 36 minutes before the accident, the wind was from 210° at 11 knots, gusting to 19 knots. The same automated station reported that, about 24 minutes after the accident, the wind was from 210° at 17 knots, gusting to 25 knots, with a peak wind reported 3 minutes after the accident from 220° at 27 knots. The pilot landed the airplane on runway 21. 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-Lateral/bank control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA424.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 ↗
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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.