NTSB CAROL · Event
Event WPR24FA313
Registry · N831AZ
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR22
Year of manufacture
2001 · 23 years old at event
TCDS
A00009CH · CIRRUS DESIGN CORP
Engine
CONT MOTOR IO-550 SERIES (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20010210
ADS-B equipped
Yes — Mode-S AB5C29
Registrant of record
847CX LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On September 27, 2024, about 1010 mountain daylight time, a Cirrus Design Corp. SR-22, N831AZ, was destroyed when it was involved in an accident near Provo, Utah. The pilot and pilot-rated passenger were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. Review of Air Traffic Control Tower communication recordings revealed that the controller instructed the pilot to enter the airport traffic pattern on downwind for runway 13. They later advised the pilot that there was an airplane on final approach to the runway and to follow that airplane. Shortly after, the pilot reported that the other airplane was in sight and the controller subsequently approved a base turn at the pilot’s discretion. As the accident airplane crossed the approach end of runway 13, the controller told the pilot to go around and that there was an airplane on the runway. The pilot replied that he was going around and that the other airplane was still on the runway. The controller asked the pilot if he was able to turn right to the downwind leg, to which the pilot replied he was able to do so. The controller cleared the pilot to land on runway 13, to which they acknowledged. No further radio transmissions from the pilot were heard. An airport surveillance video showed the first airplane approach runway 13 and perform a touch and go landing. The accident airplane then came into view and about 50 ft above ground level, entered a climb, and veered to the right before going out of view of the camera. Both airplanes appeared to be about 200 ft from each other. Preliminary ADS-B data showed the accident airplane remained within the airport traffic pattern and turned onto the downwind leg at a ground speed of about 110 knots. The data showed that a few moments later, just before the airplane initiated a right turn to the base leg for runway 13, and that the ground speed had decreased to about 80 knots. Shortly after the right turn was initiated, the ADS-B data ended over Utah Lake near the accident site. A witness in another airplane reported that they observed the accident airplane “bank sharply then stall” before it “fell into a rapid descent with 3 rotations.” The witness added that he saw the airplane’s parachute start to deploy just prior to the airplane impacting the water. The airplane came to rest submerged in about 9 ft of water about 2 miles northwest of the approach end of runway 13. The airplane plane was heavily fragmented. All major components of the airplane were recovered from the water with the exception of both flaps, ailerons and the propeller assembly. The wreckage was relocated to a secure facility for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2024_WPR24FA313.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 ↗