NTSB CAROL · Event
Event CEN22LA297
Registry · N469AK
FAA Aircraft Registry record.
Make / Model
CUB CRAFTERS INC CC18-180
Year of manufacture
2018 · 4 years old at event
Engine
LYCOMING O-360-C1G (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20180906
ADS-B equipped
Yes — Mode-S A5BB14
Registrant of record
WELLS KRIS G
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain airplane control during the go-around, which resulted in impact with terrain. Contributing to the accident was the pilot’s impairment from the effects of alcohol consumption.
Factual narrative
On July 1, 2022, about 1225 mountain daylight time, a Cub Crafters CC18-180 airplane, N469AK, sustained substantial damage when it was involved in an accident at the U.S. Air Force Academy, Colorado. The pilot sustained minor injury. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 glider tow flight. The airplane was owned, operated, and maintained by Akima Logistics Services LLC, a federal government contractor. The airplane was part of a fleet used to tow gliders for the U.S. Air Force Academy cadet glider flight training program. Civilian pilots are employed to operate the airplanes. On the day of the accident, the pilot reported for duty to assume the afternoon shift around 1145 and received the daily safety brief from the lead tow pilot. The accident occurred following the pilot’s second glider tow of the day. The pilot classified the approach to runway 16R as normal and stated that he was preparing for a wheel landing. The pilot reported that he encountered “meteorological conditions I hadn’t seen/felt before,” and the airplane began to “drift quickly left” “more forcibly than normal turning tendencies.” The pilot decided to initiate a go-around. As the airplane accelerated during the go-around, it started “turning/yawing” even though the pilot was trying to accelerate straight and level. The pilot surmised this was from the same meteorological effect that initially pushed the airplane left, and he classified it as a “wind vane effect.” The pilot noticed that the airplane seemed to yaw to the right without the wing drop characteristics of an aerodynamic stall. The airplane began descending, touched down, and came to rest inverted in a grass field. The glider tow rope remained attached to the airplane. The pilot egressed from the airplane via the cockpit door without further incident. The airplane sustained substantial damage to both wings and the empennage. The pilot reported that there were no preimpact mechanical malfunctions or failures with the airframe or the engine that would have precluded normal operation. First responders provided medical treatment to the pilot at the accident site. The first responders reported that they smelled alcohol on the pilot’s breath in the ambulance. The pilot admitted to first responders that he had consumed alcohol earlier that morning. The pilot’s evaluation upon arrival at the local hospital included a clinical serum ethanol test that was collected at 1324 and showed a serum ethanol level of 0.079 g/dL. The physician’s note documented that first responders reported that the pilot smelled like alcohol and had been drinking 8 hours before the flight. The physician documented that the pilot admitted to drinking alcohol the night before the accident date but could not state the amount that he had consumed or when he had stopped drinking, although the pilot felt that it had been more than 8 hours before flying. The physician documented alcohol intoxication among the pilot’s visit diagnoses. The FAA Forensic Sciences Laboratory performed toxicological testing of leftover specimens from the pilot’s postaccident hospital care that found ethanol at 0.057 g/dL in the pilot’s blood. The pilot’s employer subjected him to a non-Department of Transportation (DOT) breath alcohol test following the accident. According to records of this test, the test was performed at 1702, and was negative. The pilot’s employer also subjected him to a non-DOT urine drug test following the accident. According to records of this test, it was collected at 1707. A medical review officer verified the urine drug test results, reporting the test as negative for tested-for substances. The glider tow pilot had completed one flight and was returning to the airport following the second tow of the day. The pilot reported that, during the approach, he encountered a meteorological effect and the airplane drifted to the left and the pilot decided to initiate a go-around. As the airplane was accelerating during the go-around, it started “turning/yawing” even though the pilot was trying to accelerate straight and level. The pilot surmised this was from the same meteorological effect that initially pushed the airplane left. The pilot noticed that the airplane seemed to yaw to the right, the airplane began descending, touched down, and came to rest inverted in a grass field, resulting in substantial damage to both wings and the empennage. The pilot admitted to first responders that he had consumed alcohol earlier that morning. The pilot was evaluated at a hospital, where he was diagnosed with alcohol intoxication based on a serum ethanol test result of 0.079 g/dL collected about one hour after the accident. It is likely that the pilot was experiencing impairing effects of ethanol at the time of the accident. It is unknown whether ethanol’s impairing effects were worsened by altitude effects (the field elevation of the airport was about 6,500 ft above mean sea level); however, it is likely that ethanol effects increased the pilot’s risk of making serious errors and diminished his ability to effectively maintain airplane control. Thus, pilot impairment from effects of alcohol consumption likely contributed to the accident. 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-Physical-Impairment/incapacitation-Alcohol-Pilot
- — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Yaw control-Not attained/maintained
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained
- — Personnel issues-Physical-Health/Fitness-Use of alcohol-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2022_CEN22LA297.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, go-around). 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
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