NTSB CAROL · Event
Event ANC15CA031
Registry · N84116
FAA Aircraft Registry record.
Make / Model
AERONCA 7EC
Year of manufacture
1946 · 69 years old at event
Engine
CONT MOTOR C90-12F (95 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20120402
ADS-B equipped
Yes — Mode-S AB862A
Registrant of record
KOLIADKO JOSEPH I
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The instructor's delayed remedial actions, and the student pilot's failure to maintain adequate airspeed, which resulted in a stall just above the ground and the subsequent hard landing.
Factual narrative
The student pilot and his instructor were landing in a tailwheel-equipped airplane at night. The student pilot did two full stop landings on the night cross-country flight. During the first landing, the airplane stalled just above the runway, and the front left landing gear made contact with the runway first, resulting in a hard landing. The second landing was a normal, soft touchdown landing. A postflight inspection revealed that a portion of airplane's fuselage, on the left side, sustained substantial damage from the hard landing. The instructor pilot stated that there were no preaccident mechanical anomalies with the airplane that would have precluded normal operation. The student pilot and his instructor were landing in a tailwheel-equipped airplane at night. The student pilot did two full stop landings on the night cross-country flight. During the first landing, the airplane stalled just above the runway, and the front left landing gear made contact with the runway first, resulting in a hard landing. The second landing was a normal, soft touchdown landing. A postflight inspection revealed that a portion of airplane's fuselage, on the left side, sustained substantial damage from the hard landing. The instructor pilot stated that there were no preaccident mechanical anomalies with the airplane that would have precluded normal operation. 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2015_ANC15CA031.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 ↗