NTSB CAROL · Event
Event WPR10CA172
Registry · N428PA
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-181
Year of manufacture
2001 · 9 years old at event
Engine
LYCOMING O&VO-360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20010727
ADS-B equipped
Yes — Mode-S A51A9D
Registrant of record
BIRD ACQUISITION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor's failure to attain and maintain adequate airspeed while demonstrating a soft-field takeoff.
Factual narrative
The flight instructor was demonstrating a soft field takeoff to his student. During the takeoff roll, he applied full back pressure on the yoke; he heard the stall horn and he lowered the nose. As the aircraft left the ground, the flight instructor heard the stall horn a second time. The airplane's right wing began to rise as the aircraft reached an estimated altitude of 20 feet above ground level. The flight instructor checked that the throttle was full forward, but the airplane would not accelerate. As the airplane continued to turn left, it departed the left side of the runway, and the left wing impacted a runway information sign. The airplane came to a stop in the grass off the left side of the runway. The left wing's forward spar was damaged and the left fuel tank was ruptured. The right wing's outer 4 feet (estimated) was bent up and the engine's fire wall was wrinkled. The flight instructor was demonstrating a soft-field takeoff to his student. During the takeoff roll, he applied full back pressure on the yoke, heard the stall horn, and lowered the nose. As the aircraft left the ground, the flight instructor heard the stall horn a second time. The airplane's right wing began to rise as the aircraft reached an estimated altitude of 20 feet above ground level. The flight instructor checked that the throttle was full forward, but the airplane would not accelerate. As the airplane continued to turn left it departed the left side of the runway and the left wing impacted a runway information sign. The airplane came to a stop in the grass off the left side of the runway. The left wing's forward spar was damaged and the left fuel tank was ruptured. The right wing's outer 4 feet (estimated) was bent up and the engine's firewall was wrinkled. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Instructor/check pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2010_WPR10CA172.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
Browse the full corpus — academia portal ↗