NTSB CAROL · Event
Event WPR11LA458
Registry · N46BT
FAA Aircraft Registry record.
Make / Model
HUMPTON LYLE R RAF 2000 GTX SE FI
Year of manufacture
2006 · 5 years old at event
Engine
SUBARU ALL MDLS A/B (400 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20061021
ADS-B equipped
Yes — Mode-S A5976D
Registrant of record
TAYLER BARON L
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain airspeed while maneuvering, which resulted in an aerodynamic stall. Contributing to the accident was the pilot’s impairment from alcohol.
Factual narrative
On September 19, 2011, about 0850 Pacific daylight time (PDT), a Pitts S-2B airplane, N46BT, collided with the ground near Redlands, California. The private pilot, the sole occupant, sustained serious injuries. The airplane was consumed by fire and sustained substantial damage. The airplane was registered to the pilot, and operated under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91 as a personal flight. Visual meteorological conditions prevailed and no flight plan had been filed. The flight originated from the Redlands Municipal Airport, Redlands, California, about 0830. Witnesses reported that the pilot was conducting aerobatic maneuvers over the airport when the airplane impacted terrain adjacent to an airport perimeter fence. After impact, the airplane slid into an unoccupied vehicle that was parked on the shoulder of a city roadway. A post crash fire ensued. The pilot reported that he was maneuvering in the local area shortly after takeoff and that during a turn, the airplane stalled approximately 350 feet above the ground. He reported that the airspeed in the turn was slow, between 70-80 knots. The pilot attempted to recover from the stall; however, the airplane continued to descend and subsequently collided with terrain. First responders to the accident site reported that they noted an odor of alcoholic beverage when they made contact with the pilot at the accident site. About one hour after the accident a blood sample from the pilot was secured, and later tested for alcohol intoxicants. The test results showed that the pilot’s blood alcohol content (BAC)was .04 percent. During a telephone conversation after the accident with the NTSB investigator-in-charge, the pilot stated that he had consumed alcohol prior to the accident flight. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operations. According to the Federal Aviation Administration, effects of a BAC of .04% can include decreased attention, impaired judgment, and increased reaction time. It advises that "The number of serious errors committed by pilots dramatically increases at or above concentrations of 0.04% blood alcohol. This is not to say that problems don’t occur below this value. Some studies have shown decrements in pilot performance with blood alcohol concentrations as low as 0.025%." Title 14 CFR Part 91.17, Alcohol or Drugs, states, "(a) No person may act as a crewmember of a civil aircraft (1) Within 8 hours after the consumption of any alcoholic beverage; (2) While under the influence of alcohol…(4) While having an alcohol concentration of 0.04 or greater in a blood…" The pilot reported that the airplane stalled while maneuvering at a low altitude. He attempted to recover from the stall; however, the airplane continued to descend and subsequently collided with terrain. First responders to the accident site reported that they noted an odor of alcohol when they spoke to the pilot at the accident site. About one hour after the accident, a blood sample from the pilot was secured and later tested for alcohol intoxicants. The test results showed that the pilot’s blood alcohol concentration (BAC) was .04 percent. According to the Federal Aviation Administration, effects of a BAC of .04 percent can include decreased attention, impaired judgment, and increased reaction time. The pilot later reported that he had consumed alcohol prior to the accident flight. The pilot also reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operations. 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).
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- F Personnel issues-Physical-Impairment/incapacitation-Alcohol-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2011_WPR11LA458.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 ↗