NTSB CAROL · Event
Event ATL02LA122
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed during a banner tow pickup resulting in an inadvertent stall and uncontrolled descent and collision with terrain.
Factual narrative
On June 15, 2002, about 1215 eastern daylight time, a Cessna 172R, N9857F, registered to a private owner, operated by Barn Stormer as a 14 CFR Part 91 banner tow flight, crashed during a banner pick up in North Myrtle Beach, South Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage. The commercial pilot reported no injuries. The flight originated from Grand Strand Airport, North Myrtle Beach, South Carolina, at 1205. The pilot stated he departed Grand Strand Airport and remained in closed traffic to pick up a banner in the banner tow area located west of runway 05. He made an approach and missed the banner, went back around, made another approach, and missed again. He picked up the banner on the 3rd attempt. The airplane was in a nose up attitude as the banner started to come off the ground, and the airplane started to sink. He released the banner, the airplane continued to sink, and he lowered the nose. The airplane stalled, the wings were rocking back and forth, and the flight controls would not control the airplane. The airplane continued to sink until the left wing collided with the ground. The airplane came to rest on its landing gear. When the pilot exited the airplane, he observed that both wings had been damaged and the engine assembly was bent downward. The pilot stated he did not experience any anomalies with the airplane before it stalled. The pilot did not report airspeed information when the airplane began to sink, a review of the Cessna 172R Skyhawk Information Manual indicates in Section 5, Performance, Figure 5-3, Stall Speeds, with a most rearward center of gravity with flaps up that the airplane will stall at 44 KIAS or 51 KCAS with 0-degrees angle of bank. It further states altitude loss during a stall recovery may be as much as 230 feet. The pilot stated he was on his 3rd attempt to pick up a banner. The airplane was in a nose up attitude as the banner started to come off the ground. At this point the airplane started to sink. The pilot released the banner but the airplane continued to sink, and he lowered the nose. The airplane stalled and the wings were rocking back and forth. The airplane continued to sink until the left wing collided with the ground. The pilot stated he did not experienced any anomalies with the airplane before it stalled. Review of the Cessna 172R Skyhawk Information Manual indicates the airplane will stall at 44 KIAS or 51 KCAS with 0-degrees angle of bank. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_ATL02LA122.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…
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