NTSB CAROL · Event
Event FTW02CA206
Aircraft involved
Probable cause & findings
the loss of control due to the encounter with the dust devil.
Factual narrative
On July 13, 2002, approximately 1530 mountain daylight time, an Aero Commander Callair A-9B single-engine airplane, N7791V, was substantially damaged when it impacted terrain following an encounter with a dust devil during landing at the West Texas Airport near El Paso, Texas. The airplane was registered to and operated by the El Paso Soaring Society of El Paso. The airline transport pilot, sole occupant of the airplane, sustained serious injuries. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 glider tow flight. The local flight originated from the West Texas Airport, approximately 1510. The pilot reported that while attempting to land on runway 8, he saw a dust devil approximately 50 to 100 feet directly in front of him over the runway. Due to heavy rain, which had passed through the area, the dust devils were not picking up sand as usual. All he saw was a couple of sheets of flying paper. Being too low to turn, he applied full power and attempted to fly through the dust devil. When the airplane pitched up and went into a left climbing turn due to the cyclonic effect, he applied full right aileron and rudder in an attempt to control the airplane. Witnesses observed the airplane pitch up and make a 270 degree left turn. The airplane became inverted and impacted the ground on its nose, bounced, and came to rest 150 feet north of the runway on its main landing gear facing south. Examination of the airplane by the FAA inspector, who responded to the accident site, revealed that both wings were structurally damaged, and the engine was displaced into the firewall. While attempting to land, the pilot saw a dust devil approximately 50 to 100 feet directly in front of him over the runway. Being too low to turn, he applied full power and attempted to fly through the dust devil. When the airplane pitched up and went into a left climbing turn, he applied full right aileron and rudder in an attempt to control the airplane. Witnesses observed the airplane pitch up and make a 270 degree left turn. The airplane became inverted and impacted the ground on its nose, bounced, and came to rest on its main landing gear. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_FTW02CA206.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 (loss of control). 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 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation)
ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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