ERA20CA227
2020-06-19 · Churchville, Maryland, United States · None · 1 aircraft · Status: Completed
Airport 0W3
Current FAA registration · N21585
- Make / Model
- CESSNA 172M
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19740924
- ADS-B equipped
- Yes — Mode-S A1CFA3
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's improper landing flare and improper recovery from a bounced landing in gusty wind conditions, which resulted in a hard landing.
Factual narrative
The student pilot was practicing takeoffs and landings in the airport traffic pattern and had previously completed two previous successful landings while flying with his flight instructor. The flight instructor then disembarked, and the student took off for what would be his second solo flight. After one successful landing, he approached the runway for a second. His approach to final was normal and stabilized and the student transitioned to landing. Upon contact with the runway the airplane bounced and became airborne, then touched down again, but this time nosewheel first which made the airplane bounce again and became airborne. The student applied full power to go around, then hesitated, and reduced power to attempt to recover the landing. The airplane immediately descended and struck the ground hard. The student attempted to slow down by pulling back on the control wheel and simultaneously applying the brakes. The airplane veered off the left side of the runway, stopped abruptly, and tipped up onto its nose. The airplane’s left wing was substantially damaged during the accident. The operator reported that there were no mechanical failures or malfunctions of the airplane that would have precluded normal operation, nor did the student pilot or flight instructor report any in their provided written statements. The student also reported that the wind gusts on the accident landing approach were higher than the previous approaches, and while on final over the runway, “…it was as if the wind had been taken out from under the wings, resulting in the accelerated decent rate.” He added that he was reluctant to pull back on the control wheel, as a stall could have resulted. 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-Landing flare-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
- C Personnel issues-Action/decision-Action-Incorrect action performance-Student/instructed pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2020_ERA20CA227.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 ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
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Related research
Matched on aircraft type or causal vocabulary (icing, stall). All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
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- 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.
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- NASA NTRS 2019 · Contractor Report (CR) An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…