NTSB CAROL · Event
Event WPR24FA124
Aircraft involved
Factual narrative
On April 13, 2024, about 2019 Pacific daylight time, a Gulfstream Corporation 695A, N965BC, was destroyed when it was involved in an accident near San Bernardino, California. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot had planned to fly the airplane from the Stockton Metro Airport (SCK), Stockton, California to the Chino Airport (CNO), Chino, California, after the completion of recurrent training that had been conducted in the accident airplane. According to preliminary Automatic Dependent System Broadcast (ADS-B) data, the airplane departed SCK at 1902, turned to a southerly heading, and climbed to a cruise altitude of flight level (FL) 250. About 1928, the airplane turned to the southeast, and remained at FL 250 until about 1957, when it began a descent. During the descent, the airplane’s flight track deviated about 15° left, and the air traffic control (ATC) controller asked the pilot if he intended to remain on the established standard terminal arrival route. The pilot responded that the airplane’s autopilot had disengaged in turbulence, and he was “correcting.” About 2013, ADS-B data showed that the airplane was at 12,000 ft mean sea level (msl), when the pilot reported to ATC, moderate rime ice accumulation. Two additional descent clearances were issued by ATC, to 8,000 ft msl and 7,400 ft msl, respectively. The pilot reported that the icing conditions continued during the descent. The airplane descended below 7,400 ft msl and ATC instructed the pilot to climb the airplane to 7,400 ft msl, stating that the minimum vectoring altitude in that location was 7,400 ft msl. ADS-B data showed that at 2017:57, the airplane leveled off at 7,200 ft msl for about 30 seconds, before it began a rapid descent. The last recorded ADS-B target was at 2018:47, at an altitude of 2,600 ft msl. An Alert Notice (ALNOT) was issued at 2035 and a ground search was initiated. The wreckage was located on April 14, 2024, by the San Bernardino County Sherrif’s Aviation Unit in steep sloping terrain approximately 20 miles northeast of CNO, at an elevation of about 2,541 ft msl. Examination of the accident site revealed that the airplane impacted mountainous terrain near the top of a 45° sloping ridgeline within a south facing ravine. Debris was dispersed along both sides of the sloping ridgeline. The first identified point of contact (FIPC) with the ground was near the top of the sloping ridgeline. The portion of the debris field along the south facing slope was about 260 ft in length from the FIPC and was oriented on a magnetic heading of 236°. The portion of the debris field along the north facing slope was about 190 ft in length from the FIPC and was oriented on a magnetic heading of 286°. All major structural components of the airplane were observed throughout the debris field. The wreckage has been recovered to a secure location for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2024_WPR24FA124.txt.
Findings + structured fields enriched from FAA avall.mdb.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing, turbulence, autopilot). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2023 · Faculty research project
Understanding the Coupled Interactions Between Hair-Like Micromechanoreceptors and Wall Turbulence
This research focuses on understanding the interactions between turbulent flows and long (high aspect ratio), flexible hair-like microstructures or micropillars inspired by those encountered in nature…
- arXiv 2026 · arXiv preprint
Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
Political Turbulence and Aviation Safety: A Cross-National Analysis of Political Stability's Effects on Aviation Accidents
To what extent does political stability affect aviation safety? This research aims to link domestic political conditions and public safety through the consideration of aviation accident frequency.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
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