NTSB CAROL · Event
Event CHI01LA321
Registry · N47964
FAA Aircraft Registry record.
Make / Model
BOEING B75N1
Year of manufacture
1943 · 58 years old at event
Engine
CONT MOTOR W670-6N (220 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20111108
ADS-B equipped
Yes — Mode-S A5E5D0
Registrant of record
AMERICAN AIRPOWER HERITAGE FLYING MUSEUM
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot misjudged the proper alignment with the landing area. Contributing to the accident was the light conditions.
Factual narrative
On September 22, 2001, at 1940 central daylight time, a Boeing Stearman B75N1, N47964, owned and piloted by a commercial pilot, sustained substantial damage during a landing in a cornfield, which was adjacent to a sod area that ran parallel to runway 36R (6,506 feet by 100 feet, asphalt surface) at the Southern Illinois Airport (MDH), Carbondale, Illinois. Night visual meteorological conditions prevailed at the time of the accident. The flight was operating under the provisions of 14 CFR Part 91 and was not on a flight plan. The pilot and his single passenger reported no injuries. The flight departed Shelby County Airport, Shelbyville, Illinois, at 1910. According to the pilot's written statement, he was attempting to land on the sod area to the right side of runway 36R. The pilot reported, "Because of ditch to left and low light conditions approach was to right of center of sod. Approach was 35 yards too far to right and when ground was in sight for landing, the tassels of a cornfield were mistaken for grass runway. A normal 3 point full stall landing was made to the tops of corn, proceeding for 100 feet and a very slow pitch over onto nose and back." According to the manager of the air traffic control tower at MDH, the pilot requested to land on the sod area to the right side of runway 36R and the aircraft actually landed in the cornfield adjacent to the sod area on a northerly heading. The tower manager approximated the perpendicular distance from the edge of runway 36R to the accident site was 350 feet. The tower manager approximated the width of the sod area adjacent to runway 36R to be 200 feet. According to an almanac of sun data, the sun set at 1854 and the end of civil twilight was at 1920. The Southern Illinois Airport Authority (SIAA) approved takeoff and landing operations on the sod area adjacent to runway 36R for two specific pilot/aircraft combinations. The SIAA issued a memorandum to the air traffic control tower that discussed the associated limitations and provisions of the operation of aircraft on the sod area. The memo states, "These individuals [the two pilots allowed to use the sod area] have been instructed as to the usable portion of that ground and have agreed to accept full responsibility for their activities in the use of that area. The SIAA views this as an 'at your own risk' operation." The memorandum did not have any additional limitations or provisions, including the restriction of operations after civil twilight. Subsequent to the accident, the SIAA mandated that flight operations on the sod area would be during daylight hours only. The pilot was attempting a night landing on a sod area to the right side of the runway and landed approximately 150 feet to the right of the sod area in a cornfield. The pilot reported, "Because of ditch to left and low light conditions approach was to right of center of sod. Approach was 35 yards too far to right and when ground was in sight for landing, the tassels of a cornfield were mistaken for grass runway. A normal 3 point full stall landing was made to the tops of corn, proceeding for 100 feet and a very slow pitch over onto nose and back." According to an almanac of sun data, the sun set at 1854 and the end of civil twilight was at 1920. The Southern Illinois Airport Authority (SIAA) approved takeoff and landing operations on the sod area adjacent to runway 36R for two specific pilot/aircraft combinations. The memorandum did not have any additional limitations or provisions, including the restriction of operations after civil twilight. Subsequent to the accident, the SIAA mandated that all flight operations on the sod area would be during daylight hours only. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_CHI01LA321.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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