ERA10CA380
2010-07-27 · Shirley, New York, United States · None · 1 aircraft · Status: Completed
Airport HWV
Current FAA registration · N757ZN
- Make / Model
- CESSNA 152
- Year of manufacture
- 1977 · 33 years old at event
- Engine
- LYCOMING 0-235 SERIES (115 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19770804
- ADS-B equipped
- Yes — Mode-S AA3656
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot’s improper recovery from a bounced landing.
Factual narrative
According to the student pilot, the accident flight was her first solo flight. As the airplane approached runway 33 for a third landing, the student pilot maintained an airspeed of 60 knots and was concentrating on "getting the nose in the correct position." When the airplane first touched down, "it bounced" and "the nose went up enough to slow [the airplane] down to put it into a stall." When the airplane landed a second time, the nose landing gear collapsed and the propeller struck the runway, which resulted in substantial damage to the engine firewall. The student pilot reported no mechanical anomalies with the airplane prior to the accident. During a subsequent examination of wreckage, a Federal Aviation Administration inspector also found no preexisting anomalies with the airplane. The student pilot noted that her total flight experience was approximately 56 hours; all of which were in the same make and model as the accident airplane. The winds reported at the airport about the time of the accident were variable at 6 knots. According to the student pilot, the accident flight was her first solo flight. As the airplane approached runway 33 for a third landing, the student pilot maintained an airspeed of 60 knots and was concentrating on "getting the nose in the correct position." When the airplane first touched down, "it bounced" and "the nose went up enough to slow [the airplane] down to put it into a stall." When the airplane landed a second time, the nose landing gear collapsed and the propeller struck the runway, which resulted in substantial damage to the engine firewall. The student pilot reported no mechanical anomalies with the airplane prior to the accident. During a subsequent examination of wreckage, a Federal Aviation Administration inspector also found no preexisting anomalies with the airplane. The student pilot noted that her total flight experience was approximately 56 hours; all of which were in the same make and model as the accident airplane. The winds reported at the airport about the time of the accident were variable at 6 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Action/decision-Action-Incorrect action performance-Student pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Incorrect use/operation - C
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA10CA380.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 or causal vocabulary (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
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- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
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- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
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- 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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…