ERA24LA188
2024-04-18 · Stoneville, North Carolina, United States · None · 1 aircraft · Status: Completed
Airport SIF
Current FAA registration · N7921G
- Make / Model
- CESSNA 172L
- Year of manufacture
- 1970 · 54 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19701210
- ADS-B equipped
- Yes — Mode-S AAC1F5
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot’s improper landing flare, which resulted in a bounced, hard landing.
Factual narrative
The student pilot and flight instructor initially flew together on the day of the accident with the intention of practicing pattern work and landings, with the possibility of the student pilot performing her first solo flight given that the conditions were favorable. The student pilot first performed three circuits of the traffic pattern, with the instructor in the airplane, without incident. The flight instructor characterized that the student’s landings were “good,” and her patterns were consistent. The windsocks at the approach end of the runway were limp, indicating low wind. After the third landing, the flight instructor endorsed the student for solo flight and her first solo landing was uneventful. The student pilot described that when she was coming in for her second solo landing, she heard other pilots calling in over the radio saying they were on final approach to land, and she wanted to get out of the way as soon as possible. Also, during her landing, the precision approach path indicator was not on, and she had difficulty with her depth perception. She realized that she was too high and fast coming in on short final. The airplane then struck the runway and porpoised 4-times. She was subsequently unable to steer the airplane using the rudder pedals and the airplane was towed back to the ramp. Postaccident examination of the airplane revealed that the fuselage was substantially damaged. The operator reported that there were no preimpact mechanical malfunctions or failures of the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2024_ERA24LA188.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 ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (icing). 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.
- arXiv 2026 · arXiv preprint Enabling Beyond-Visual-Line-of-Sight Drones Operation over Open RAN 5G Networks with Slicing
Among the foretold claims of the transition from 5G to 6G, Beyond-Visual-Line-of-Sight (BVLoS) drone operation has emerged as a prominent Internet-of-Robots enabler.
- NASA NTRS 2026 · Contractor Report (CR) Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…