GAA16CA361
2016-06-21 · Lancaster, Ohio, United States · None · 1 aircraft · Status: Completed
Airport LHQ
Current FAA registration · N19820
- Make / Model
- CESSNA 172M
- Year of manufacture
- 1972 · 44 years old at event
- Engine
- LYCOMING O-320-E2D (150 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20081205
- ADS-B equipped
- Yes — Mode-S A1889A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper landing flare in gusting wind conditions, which resulted in a hard landing.
Factual narrative
The student pilot reported that the purpose of the flight was to practice flight maneuvers. He recalled that upon conclusion of the maneuver practice, he made a normal approach to runway 28. He reported that during the landing flare he encountered a crosswind gust, the airplane floated, and the airplane landed hard. He recalled that after the hard landing, he was unsatisfied with his landing performance. The student pilot reported that he decided to takeoff, stayed in the pattern, landed with full flaps and more airspeed, and accomplished "a controlled, more smooth touchdown." However, when he showed up for his next flight three days later, he was informed that the airplane sustained substantial damage to the firewall. The pilot reported that there were no mechanical failures or anomalies with the airplane during his flight that would have prevented normal flight operations. The meteorological aerodrome report at the accident airport about the time of the accident indicated the wind direction was out of 270 degrees true at 9 knots, gusting to 19 knots. The student pilot reported that the purpose of the flight was to practice flight maneuvers. He recalled that upon conclusion of the maneuver practice, he made a normal approach to runway 28. He reported that during the landing flare he encountered a crosswind gust, the airplane floated, and the airplane landed hard. He recalled that after the hard landing, he was unsatisfied with his landing performance. The student pilot reported that he decided to takeoff, stayed in the pattern, landed with full flaps and more airspeed, and accomplished "a controlled, more smooth touchdown." However, when he showed up for his next flight three days later, he was informed that the airplane sustained substantial damage to the firewall. The pilot reported that there were no mechanical failures or anomalies with the airplane during his flight that would have prevented normal flight operations. The meteorological aerodrome report at the accident airport about the time of the accident indicated the wind direction was out of 270 degrees true at 9 knots, gusting to 19 knots. 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-Pitch control-Not attained/maintained - C
- 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-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on equipment
Verbatim from NTSB's published report. Source file
NTSB_2016_GAA16CA361.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.