NTSB CAROL · Event
Event LAX95LA094
Aircraft involved
Probable cause & findings
the pilot's improper compensation for the prevailing wind conditions, and his improper remedial action by raising the flaps before applying the power. The downdraft was a factor.
Factual narrative
On February 3, 1995, at 1117 hours mountain standard time, a Cessna 152, N46874, collided with the terrain short of runway 03 at Sedona Airport, Sedona, Arizona. The pilot was completing a visual flight rules personal flight. The airplane, operated by Scottsdale Flyers, Scottsdale, Arizona, sustained substantial damage. The certificated private pilot and his passenger received minor injuries. Visual meteorological conditions prevailed. The flight originated at Scottsdale Airport at 1010 hours. A Federal Aviation Administration (FAA) inspector reported that the pilot said he encountered a "severe downdraft" while on final approach. The pilot could not arrest the downdraft and the airplane collided with the down-sloping terrain short of the runway threshold. The pilot repeated his statement in the aircraft accident report. He added, however, that while on final approach, the flaps were fully extended (30 degrees). When the airplane encountered the downdraft, he raised the flaps to 20 degrees, applied full power, and then turned off the carburetor heat. The pilot raised the nose to attain the best angle of climb (Vx) airspeed, but without success; the airplane continued descending. He continued to raise the nose to arrest the descent until the stall warning horn sounded. At this point, the pilot lowered the airplane nose and the airplane collided with the terrain. The airport is situated on a mesa and the threshold of runway 03 is about 150 feet northeast of the mesa drop-off. The airport manager said in a telephone interview conducted on April 25, 1995, that several airplanes landed at the airport before and after the accident. He said that the UNICOM operator advised all arriving airplanes of the prevailing strong winds. The manager also said the pilot told him that he intended to fly the approach above the operating visual approach slope indicator and land beyond the threshold. The pilot also said that "he lost control of the airplane." THE AIRPORT UNICOM ADVISED THE PILOT THAT STRONG WINDS EXISTED AT THE AIRPORT WHICH IS SITUATED ON TOP OF A MESA. WHILE ON FINAL APPROACH, WITH THE FLAPS FULLY EXTENDED, THE FLIGHT ENCOUNTERED SEVERE DOWNDRAFTS. THE PILOT IMMEDIATELY RAISED THE FLAPS TO 20 DEGREES, APPLIED FULL POWER, AND THEN RAISED THE NOSE TO ATTAIN THE BEST ANGLE OF CLIMB AIRSPEED. THE AIRPLANE CONTINUED TO DESCEND UNTIL IT COLLIDED WITH THE TERRAIN. THE PILOT SAID THE AIRPLANE DID NOT EXPERIENCE ANY PREIMPACT MALFUNCTIONS OR FAILURES. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_LAX95LA094.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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