CHI88FA188
1988-08-03 · FLUSHING, Michigan, United States · Fatal · 1 aircraft · Status: Completed
Airport 3DA
Current FAA registration · N2956Z
- Make / Model
- BELLANCA 7ECA
- Year of manufacture
- 1978 · 10 years old at event
- Engine
- LYCOMING 0-235 SERIES (115 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19780405
- ADS-B equipped
- Yes — Mode-S A30B4F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
PILOT'S PHYSICAL INCAPACITATION DUE TO A CORONARY SEIZURE, WHICH RESULTED IN A LOSS OF AIRCRAFT CONTROL, AND A STALL/SPIN INTO THE GROUND.
Factual narrative
SHORTLY AFTER TAKEOFF, AS THE AIRPLANE WAS CLIMBING THRU ABOUT 100 TO 200 FT ABOVE THE GROUND, IT WAS OBSERVED TO PITCH UP, THEN BANK RIGHT & NOSED DOWN IN WHAT WAS ESTIMATED TO BE A 3/4 TURN SPIN BEFORE IMPACTING THE GROUND. NO PREIMPACT MALFUNCTION OR FAILURE OF THE AIRCRAFT STRUCTURE OR ENGINE WAS FOUND. A PATHOLOGICAL EXAM OF THE PILOT REVEALED EXTENSIVE CHEST INJURIES AND AN ACUTE OCCLUSION OF THE LEFT ANTERIOR DESCENDING CORONARY ARTERY. THE CORONER BELIEVED THE PILOT SUFFERED A CORONARY SEIZURE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1988_CHI88FA188.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
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- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
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- 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…