NTSB CAROL · Event
Event CHI89FA117
Aircraft involved
Probable cause & findings
IMPROPER PLANNING/DECISION OF THE PILOT, WHICH RESULTED IN FUEL EXHAUSTION FROM AN INADEQUATE SUPPLY OF FUEL, AND HIS FAILURE TO MAINTAIN FLYING SPEED DURING A FORCED LANDING, WHICH RESULTED IN A STALL AND SUBSEQUENT IMPACT WITH THE GROUND.
Factual narrative
THE AIRCRAFT HAD BEEN PARKED FOR 14 MONTHS AND DID NOT HAVE A CURRENT ANNUAL INSPECTION WHEN THE OWNER/PILOT TOOK IT FOR A FLIGHT. NO KNOWN WITNESSES SAW THE AIRCRAFT TAKEOFF. SUBSEQUENTLY, THE AIRCRAFT IMPACTED IN A FIELD JUST NORTH OF THE AIRPORT. IT WAS FOUND WHEN A MOTORIST SAW A DUST CLOUD IN THE FIELD & PROCEEDED TO INVESTIGATE. AN EXAM OF THE CRASHSITE REVEALED THE ACFT HAD IMPACTED JUST NORTHEAST OF WHERE IT HAD COME TO REST. THE AIRCRAFT WAS EXTENSIVELY DAMAGED DURING IMPACT. BOTH PROP BLADES WERE BENT AFT & NEITHER HAD CHORDWISE POLISHING OR SCRATCHES. NO USABLE FUEL WAS FOUND IN THE AIRCRAFT. ALTHOUGH THE FUEL PUMP FILTER WAS WET & THE LINES WERE BROKEN BETWEEN THE GASCOLATOR & CARBURETOR, NO FUEL WAS FOUND IN THE LINES OR ELECTRIC FUEL PUMP. THE ACCIDENT OCCURRED ON A DAY WHEN THE ARPT WAS UNATTENDED & FUEL WAS NOT AVAILABLE. A TOXICOLOGY CHECK SHOWED NO ALCOHOL IN THE PILOT'S BLOOD. ALTHOUGH HIS KIDNEY TISSUE HAD AN ALCOHOL LEVEL OF 0.056%, THE TOXICOLOGY REPORT INDICATED THE ALCOHOL WAS '. . . DUE TO TISSUE DECOMPOSITION OR CONTAMINATION.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1989_CHI89FA117.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, fuel exhaustion). 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 ↗