NTSB CAROL · Event
Event MIA98LA217
Registry · N29927
FAA Aircraft Registry record.
Make / Model
WACO UPF-7
Year of manufacture
1940 · 58 years old at event
Engine
CONT MOTOR W670 SERIES (250 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19620417
ADS-B equipped
Yes — Mode-S A319A7
Registrant of record
KELLER JAMES E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A loss of engine power due to undetermined reasons, resulting in an inadvertent stall at too low an altitude to allow recovery.
Factual narrative
On August 3, 1998, about 1156 eastern daylight time, a Waco UPF-7, N29927, registered to M and F Flying Inc, crashed near Key West, Florida, while on a Title 14 CFR Part 91 banner towing flight. Visual meteorological conditions were reported and no flight plan was filed. The airplane was destroyed. The airline transport-rated pilot reported minor injuries. The flight had originated from Key West International Airport, Florida, at 1125. According, to the pilot he departed Key West International Airport, Florida, for a routine banner tow. The pilot stated "he was coming in for the banner drop with the power set at around 1600 RPM for the descent. He descended to around 75 feet and when he passed over the banner site he released the banner." The pilot applied full throttle in an attempt to gain airspeed and altitude for the climb out, but the engine did not respond to throttle input. The pilot then stated that he pumped the throttle, but still got no response. According to the pilot, "he decided to start a right turn to try to land on runway 9...and he was two thirds of the way through the turn when the right wing dropped and the aircraft nosed into the runway from an altitude of about 30 feet." According to FAA inspector, "the pilot made a tight right turn to try to land on runway 9,stalled the airplane, spun in, and impacted on the runway about 500 feet from the west end, nose down, and on a heading of about 130 degrees. Upon impact on the runway the airplane caught fire." The pilot stated to FAA inspectors that "he did not apply any carburetor heat on his approach nor when the engine did not respond." Another company pilot stated that "he had flown the aircraft the day before and it was operating normally." Examination of the airplane and engine did not reveal any discrepancies or malfunctions during preflight or postcrash. The pilot was approaching for a banner drop, the power was at a low power setting. The pilot released the banner, at an altitude of about 75 feet, applied full power, and received no response from the engine. He then pumped the throttle and again no response. He made a right turn in an attempt to land on runway 9. The airplane stalled, spun in, and impacted the runway nose down. The pilot state that 'he did not apply carburetor heat.' No discrepancies were found with the engine or airframe. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_MIA98LA217.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 ↗