Analysis of the Learjet 60 (N722BD) Air Crash

Aircraft may encounter updrafts, downdrafts, turbulence, icing, and their interactions under complex meteorological conditions, producing significant changes in vertical motion. Traditional aviation dynamics describes these phenomena through aerodynamics, fluid mechanics, and the six-degree-of-freedom equations of aircraft motion. However, when continuous airflow data, aircraft attitude data, and complete force information at the accident site are unavailable, it is difficult to uniquely determine the specific dynamic cause of anomalous aircraft motion from limited flight-track data alone. This paper takes the Learjet 60 (N722BD) accident that occurred near Florida, USA, on November 1, 2026, as its research background. It first discusses, from classical aviation dynamics, the effects of updrafts, downdrafts, and unsteady airflow on aircraft vertical motion. It then introduces the concept of local energy-field intensity proposed by Spacetime Ladder Theory (STLT) and attempts to establish a preliminary quantitative connection between changes in aircraft vertical motion and local energy-field intensity. Based on currently public ADS-B altitude data, this paper selects a flight-time window before the accident and obtains an average vertical velocity estimate of approximately . Under a further simplified model in which vertical velocity changes to zero within three seconds, an acceleration-change amplitude of approximately is obtained. If the conditional correspondence in the STLT model is further adopted, and the background field intensity corresponding to Earth’s orbital motion is used as a comparison benchmark, the local energy-field intensity is approximately 343 times that background value. This paper emphasizes that this value is a rough estimate based on simplified kinematic assumptions and a specific STLT correspondence. It is not a direct measurement of the energy field at the accident site, nor can it prove that a local energy-field anomaly was the cause of the accident. The main purpose of this paper is not to make a definitive attribution of the accident, but to propose a research direction that can be further mathematized, observed, and falsified: incorporating local energy-field intensity and its spatial variation into the candidate explanatory framework for anomalous aircraft motion.

Authors

Publication Details

Journal
Zenodo (CERN European Organization for Nuclear Research)
Published
2026-11-03
DOI
https://doi.org/10.5281/zenodo.23925514
Primary Topic
Aerospace and Aviation Technology
Type
preprint
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preprint

Analysis of the Learjet 60 (N722BD) Air Crash

binggong chang
Zenodo (CERN European Organization for Nuclear Research)
Aerospace and Aviation Technology
preprint

Analysis of the Learjet 60 (N722BD) Air Crash

binggong chang
preprint en

Abstract

Aircraft may encounter updrafts, downdrafts, turbulence, icing, and their interactions under complex meteorological conditions, producing significant changes in vertical motion. Traditional aviation dynamics describes these phenomena through aerodynamics, fluid mechanics, and the six-degree-of-freedom equations of aircraft motion. However, when continuous airflow data, aircraft attitude data, and complete force information at the accident site are unavailable, it is difficult to uniquely determine the specific dynamic cause of anomalous aircraft motion from limited flight-track data alone. This paper takes the Learjet 60 (N722BD) accident that occurred near Florida, USA, on November 1, 2026, as its research background. It first discusses, from classical aviation dynamics, the effects of updrafts, downdrafts, and unsteady airflow on aircraft vertical motion. It then introduces the concept of local energy-field intensity proposed by Spacetime Ladder Theory (STLT) and attempts to establish a preliminary quantitative connection between changes in aircraft vertical motion and local energy-field intensity. Based on currently public ADS-B altitude data, this paper selects a flight-time window before the accident and obtains an average vertical velocity estimate of approximately . Under a further simplified model in which vertical velocity changes to zero within three seconds, an acceleration-change amplitude of approximately is obtained. If the conditional correspondence in the STLT model is further adopted, and the background field intensity corresponding to Earth’s orbital motion is used as a comparison benchmark, the local energy-field intensity is approximately 343 times that background value. This paper emphasizes that this value is a rough estimate based on simplified kinematic assumptions and a specific STLT correspondence. It is not a direct measurement of the energy field at the accident site, nor can it prove that a local energy-field anomaly was the cause of the accident. The main purpose of this paper is not to make a definitive attribution of the accident, but to propose a research direction that can be further mathematized, observed, and falsified: incorporating local energy-field intensity and its spatial variation into the candidate explanatory framework for anomalous aircraft motion.

Zenodo (CERN European Organization for Nuclear Research)
Aerospace and Aviation Technology
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Analysis of the Learjet 60 (N722BD) Air Crash — binggong chang · Zenodo (CERN European Organization for Nuclear Research) (2026) | TGRS Research Map | TGRS