NTSB CAROL · Event
Event GAA16CA002
Aircraft involved
Probable cause & findings
The pilot's exceedance of the critical angle of attack in turbulent and downdraft conditions, which resulted in an aerodynamic stall and collision with terrain on final approach.
Factual narrative
The pilot reported that during his first approach to land he elected to go-around due to the crab angle and buffeting. On the second approach, he encountered downdrafts and moderate turbulence again on short final and applied power to go-around. During the go-around, the airplane continued to sink and impacted a cliff about 250 feet short of the runway threshold, and ultimately came to rest at the bottom of the cliff near a road. The fuselage and both wings sustained substantial damage. According to the airport manager, when the airplane was on final approach he announced on the common traffic advisory frequency, "wind 250 at 11 and use caution for down drafts and turbulence on short final." The accident pilot acknowledged the transmission. The airport manager continued to observe the airplane and witnessed the pitch angle continuously increase on final approach, and then he heard the engine power increase. Subsequently, the airport manager witnessed the airplane "stall" and "fall from view." The pilot reported there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot reported that during his first approach to land he elected to go-around due to the crab angle and buffeting. On the second approach, he encountered downdrafts and moderate turbulence again on short final and applied power to go-around. During the go-around, the airplane continued to sink and impacted a cliff about 250 feet short of the runway threshold, and ultimately came to rest at the bottom of the cliff near a road. The fuselage and both wings sustained substantial damage. According to the airport manager, when the airplane was on final approach he announced on the common traffic advisory frequency, "wind 250 at 11 and use caution for down drafts and turbulence on short final." The accident pilot acknowledged the transmission. The airport manager continued to observe the airplane and witnessed the pitch angle continuously increase on final approach, and then he heard the engine power increase. Subsequently, the airport manager witnessed the airplane "stall" and "fall from view." The pilot reported there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Downdraft-Ability to respond/compensate
- — Environmental issues-Conditions/weather/phenomena-Turbulence-Terrain induced turbulence-Response/compensation
Verbatim from NTSB's published report. Source file
NTSB_2015_GAA16CA002.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, turbulence). 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 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.
- NTSB Aircraft Accident Reports 2021 · Accident report
Crash of Atlas Air Flight 3591, Boeing 767-300 (N1217A)
Atlas Air 3591 crashed into Trinity Bay, Texas, February 23, 2019. Investigation of the in-flight loss-of-control crash of Atlas Air 3591 into Trinity Bay, Texas.
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA)
Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint
Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Aerodynamic prediction of glaze ice accretion on airfoils and wing is studied using the Reynolds-averaged Navier-Stokes method.
- NASA NTRS 2019 · Conference Paper
Prediction of stall and post-stall behavior of airfoils at low and high Reynolds numbers
An interactive boundary-layer method, together with the e(super n)-approach to the calculation of transition, has been used to predict the stall and post-stall behavior of airfoils at low and high Rey…
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