NTSB CAROL · Event
Event ERA13CA324
Registry · N5815V
FAA Aircraft Registry record.
Make / Model
BOEING B75N1
Year of manufacture
1941 · 72 years old at event
Engine
LYCOMING R680 (215 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19811014
ADS-B equipped
Yes — Mode-S A77CBA
Registrant of record
DEBS RAYMOND E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s decision to initiate a stall maneuver at a low altitude, which resulted in an uncontrolled descent and inadvertent collision with trees and terrain.
Factual narrative
After making a low pass over the airport, the pilot of the vintage aerobatic biplane initiated a “stall turn” in order to reverse direction. During the climb portion of the maneuver, the airplane “did not achieve the required altitude for a safe recovery due to the extra weight of [the] passenger.” During the descent and attempted recovery from the maneuver, the right wing impacted a tree and the airplane subsequently impacted the ground, and came to rest inverted. A postaccident examination of the airplane revealed substantial damage to the upper and lower wings, fuselage, and vertical stabilizer. The pilot reported no preaccident mechanical malfunctions or failures of the airplane that would have precluded normal operation. After making a low pass over the airport, the pilot of the vintage aerobatic biplane initiated a “stall turn” in order to reverse direction. During the climb portion of the maneuver, the airplane “did not achieve the required altitude for a safe recovery due to the extra weight of [the] passenger.” During the descent and attempted recovery from the maneuver, the right wing impacted a tree and the airplane subsequently impacted the ground, and came to rest inverted. A postaccident examination of the airplane revealed substantial damage to the upper and lower wings, fuselage, and vertical stabilizer. The pilot reported no preaccident mechanical malfunctions or failures of 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-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Incorrect use/operation - C
Verbatim from NTSB's published report. Source file
NTSB_2013_ERA13CA324.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 ↗