NTSB CAROL · Event
Event FTW94LA064
Aircraft involved
Probable cause & findings
AN INADVERTENT STALL DURING INITIAL CLIMB FOLLOWING TAKEOFF. A FACTOR WAS FAILURE BY THE PILOT TO MAINTAIN DIRECTIONAL CONTROL.
Factual narrative
On January 13, 1994, at 1200 mountain standard time, a Bellanca 8KCAB-180, N2974W, was destroyed when it impacted the ground at the Colorado Springs, Colorado, Airport, following takeoff. The pilot received minor injuries, his passenger no injuries. Visual meteorological conditions prevailed and no flight plan was filed for this local area personal flight. According to the pilot, aircraft acceleration during the takeoff roll appeared to be normal and some right rudder was required to track the centerline. The pilot reported the following in the enclosed report: "After the tail came up and the main wheels had just lifted off the airplane began to slip rather rapidly to the left. I attempted to correct with right rudder but was not able to stop the drift as my attention was diverted by the VASI lights which we were headed towards. I raised the nose slightly to clear the light structures. At this point the airplane was traveling at an angle of about 45 degrees to the runway with the nose only slightly up." "I was about to began a gentle turn to the right to parallel the runway and continue the takeoff when suddenly the nose pitched up then dropped as the airplane banked left. This surprised me as I had not commanded the pitch up. The airplane descended in a left bank from about 50 feet and impacted on the left wing tip and nose." According to the attached incident reports supplied by the Colorado Springs Police Department, and the Colorado Springs Department of Transportation, Aviation Division, the aircraft began to track left during the takeoff roll and departed the side of the runway prior to becoming airborne. Enclosed reports supplied by the above, indicate that the aircraft was airborne for a distance of 231 feet parallel to the runway and 264 feet at a 90 degree angle to the runway. Both reports provide information that the aircraft impacted on the nose and left wing, and began to burn at impact. The wind reported by Colorado Springs Tower at the time of the accident was 190 degrees at 8 knots, which was calculated to be a 3 knot 90 degree cross wind component. DURING TAKEOFF ROLL, THE AIRCRAFT DEPARTED THE LEFT SIDE OF THE RUNWAY AND THEN BECAME AIRBORNE. AFTER THE LOSS OF DIRECTIONAL CONTROL, THE AIRPLANE PITCHED UP AND ROLLED LEFT FOLLOWED BY AN IMPACT ON THE LEFT WING AND NOSE IN THE AIRPORT INFIELD. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_FTW94LA064.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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