CEN20LA392
2020-09-13 · Cottage Grove, Minnesota, United States · Fatal · 1 aircraft · Status: Completed
Airport SGS
Current FAA registration · N8488L
- Make / Model
- CESSNA 172I
- Year of manufacture
- 1968 · 52 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19680330
- ADS-B equipped
- Yes — Mode-S ABA10C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A steep descent and impact with terrain for reasons that could not be determined based on the available information.
Factual narrative
HISTORY OF FLIGHTOn September 13, 2020, at 1432 central daylight time, a Cessna 172, N8488L, was destroyed when it was involved in an accident near Cottage Grove, Minnesota. The flight instructor and two passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight. According to the operator, the accident flight was a “discovery flight” arranged by the passenger for his girlfriend. Discovery flights typically included 1/2 hour of ground training and a preflight inspection of the airplane, followed by the flight, during which the front-seat passenger operated the controls to the extent possible. The male passenger was seated in the right rear seat, the female passenger was seated in the left front seat, and the flight instructor was seated in the right front seat. According to Automatic Dependent Surveillance-Broadcast (ADS-B) data, the airplane departed about 1428 and proceeded southbound until it crossed the Mississippi River, then it turned to a southeast heading. The last return from the airplane was at 1432, over Lower Grey Cloud Island at an altitude of about 1,900 ft and speed of 101 mph. The flight profile view revealed a sharp descent followed by a sharp ascent as the airplane approached Lower Grey Cloud Island; the airplane subsequently entered a steep descent that continued until impact. An aircraft performance study based on the ADS-B information indicated that the airplane lost over 1,000 ft of altitude in seven seconds: a descent rate of over 8,000 ft per minute, before impact. The pilot of another airplane, inbound to the departure airport, had a Go-Pro video camera operating in the cockpit and captured the accident airplane as it descended. Although eagles or geese were seen in the area, there was no evidence to indicate that the accident airplane collided with any of these birds. WRECKAGE AND IMPACT INFORMATIONThe wreckage was located in 70-foot-deep water and was examined at a secure facility following recovery. All control cables failed at or near their cockpit connections and the failures were consistent with overload. The cables were traced from the cabin area to their respective flight control surfaces. Both wings displayed accordion-type compression damage aft to the main spar, consistent with high-speed impact. The left horizontal stabilizer had more impact damage than the right horizontal stabilizer. The vertical stabilizer, although straight, was impact damaged, but the anticollision light on top of the tail was intact, consistent with the airplane being upright upon impact. The damaged propeller blades were bent aft into the engine compartment. The examination of the engine revealed no anomalies that would have precluded normal engine operation. MEDICAL AND PATHOLOGICAL INFORMATIONThe Ramsey County Medical Examiner performed the CFI’s autopsy; cause of death was multiple traumatic injuries, aircraft accident, and his manner of death was accident. The Federal Aviation Administration Forensic Sciences Laboratory identified ethanol at 0.051 g/dL in cavity blood and did not detect ethanol in urine. The accident flight was a “discovery flight” arranged by the rear seat passenger for his girlfriend, the front seat passenger. A flight instructor was seated in the right front seat. Flight track information revealed that, about four minutes after departure at an altitude of about 1,900 ft, the airplane entered a steep descent that continued until water contact. The airplane was destroyed when it impacted the water. Examination of the airplane revealed no evidence of mechanical anomalies that would have precluded normal operation, and no evidence of a bird strike. Visual meteorological conditions were present in the area at the time of the accident. Available medical information provided no evidence that the CFI had any medical condition, substance use, or toxic exposure that contributed to the accident. Based on the absence of detected ethanol in the CFI’s urine, it is likely that ethanol detected in his cavity blood was from sources other than ingestion. Given the available information, the reason for the airplane’s impact with terrain could not be determined. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Flight crew
- — Not determined-Not determined-(general)-(general)-Unknown/Not determined
Verbatim from NTSB's published report. Source file
NTSB_2020_CEN20LA392.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- Embry-Riddle Scholarly Commons 2023 · Conference paper Validation of Training Satisfaction Survey
The Training Satisfaction Survey (TSS) was developed as part of a larger project to examine the features of Virtual Reality software and supporting devices as a training program on visual illusions an…
- Semantic Scholar 2021 · Article (Data in Brief) Cockpit voice recorder transcript data: Capturing safety voice and safety listening during historic aviation accidents
Cockpit Voice Recorder (CVR) transcripts capture audio data within cockpit environments. This aids the investigation of causal factors contributing to aviation accidents by revealing communication and…
- Semantic Scholar 2021 · Article (Safety Science) Safety voice and safety listening during aviation accidents: Cockpit voice recordings reveal that speaking-up to power is not enough
Abstract Safety voice is theorised as an important factor for mitigating accidents, but behavioural research during actual hazards has been scant.