NTSB CAROL · Event
Event CEN21FA424
Registry · N19BB
FAA Aircraft Registry record.
Make / Model
BOEING A75
Engine
P & W R-985-AN-1 (450 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19930830
ADS-B equipped
Yes — Mode-S A165ED
Registrant of record
BOTTOLENE BRIAN J
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s loss of control during an aerobatic maneuver, resulting in the airplane impacting terrain.
Factual narrative
HISTORY OF FLIGHTOn September 17, 2021, about 0800 central daylight time, a Boeing A75 airplane, N19BB, was substantially damaged when it was involved in an accident near Delta, Colorado. The pilot sustained fatal injuries. The flight was operated under the provisions of Title 14 Federal Code of Regulations Part 91 as a personal flight. The airplane took off from runway 3 at Blake Field Airport (AJZ), Delta, Colorado. Two witnesses observed the airplane climb out and begin aerobatic maneuvers about 5 miles to the northeast of AJZ. Both witnesses reported that the airplane began a loop maneuver, and at the top of the loop while inverted, the airplane entered a flat spin. They observed the airplane recover from that spin. The airplane then gained altitude and they observed the airplane begin another loop maneuver. At the top of that loop, while inverted, the airplane entered another flat spin, but this time the pilot did not recover. The airplane impacted rugged, sloped terrain about 5 miles to the northeast of AJZ. First responders located the airplane wreckage and notified authorities. There were no radio or distress calls heard from the pilot. The witnesses reported that the engine could be heard running during the descent to the point of impact. AIRCRAFT INFORMATIONAccording to an acquaintance of the pilot, who also witnessed the accident, he and the pilot flew the airplane to AJZ a few days before the accident flight. The acquaintance stated that the airplane operated normally. AIRPORT INFORMATIONAccording to an acquaintance of the pilot, who also witnessed the accident, he and the pilot flew the airplane to AJZ a few days before the accident flight. The acquaintance stated that the airplane operated normally. WRECKAGE AND IMPACT INFORMATIONThe wreckage was found resting inverted on a 45-degree sloped hill. The fuselage was oriented downslope and crushed inward from impact forces. The engine was partially separated from its mounts. The empennage section was bent rearward, the upper wings were bent upward, and lower wings were separated from their respective mounting braces, consistent with a flat impact. One blade of the two-bladed propeller had no damage while the other blade was bent aft 45o with no twisting. Flight control continuity was confirmed from the cockpit to all flight control surfaces. The engine throttle control was found in the idle position. Engine rotation continuity (compression resistance) was confirmed. The smell of fuel was present. The airplane was not equipped with inverted fuel or oil supply systems. MEDICAL AND PATHOLOGICAL INFORMATIONThe Pathology Group, P.C., Grand Junction, Colorado, performed the pilot’ s autopsy as authorized by the Delta County Coroner’s Office, Delta, Colorado. According to the pilot’s autopsy report, his cause of death was multiple blunt force injuries, and his manner of death was accident. The autopsy did not identify significant natural disease. The Federal Aviation Administration Forensic Sciences laboratory performed toxicology testing of postmortem specimens from the pilot. Diphenhydramine, famotidine, desloratadine, and pseudoephedrine were detected in cavity blood and urine. The pilot took off and proceeded to an area northeast of the airport where he began performing aerobatic maneuvers. Witnesses reported that the airplane began a loop maneuver and, at the top of the loop while inverted, the airplane entered a flat spin. They observed the airplane recover from the spin. The airplane then gained altitude and entered another loop. At the top of that loop, while inverted, the airplane entered another flat spin, but this time the pilot did not recover. The airplane descended to impact with rugged terrain. The witnesses reported that the engine could be heard running during the descent to the point of impact. A postaccident examination revealed no preaccident failures or malfunctions with the airplane that would have precluded normal operation. The pilot had used the sedating antihistamine diphenhydramine, which has a potential to cause cognitive and psychomotor slowing and drowsiness. There was insufficient evidence to determine whether the pilot was experiencing impairing diphenhydramine effects at the time of the crash, and no specific evidence that pilot impairment contributed to the crash. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Yaw control-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2021_CEN21FA424.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.
Browse the full corpus — academia portal ↗