GAA16CA181
2016-04-03 · Orangeburg, South Carolina, United States · None · 1 aircraft · Status: Completed
Airport OGB
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the takeoff, resulting in a runway excursion and a nose over.
Factual narrative
The pilot reported while practicing take offs and landings, he made a standard approach and landing to runway 35. On takeoff, he reduced the flaps to zero degrees and he reported that the airplane was under control and over the runway centerline. After he applied full power and right rudder before lifting off the ground, the airplane started turning to the left sharply. He applied additional right rudder, he reduced the power, and applied full brakes. The airplane departed the runway to left into a swamp and nosed over. The airplane sustained substantial damage to the right wing and the firewall. The pilot verified that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot reported that the wind velocity at the accident site was 6 to 7 knots and the wind direction was 330 degrees. The weather reporting facility at the accident site reported that about 3 minutes after the accident time that the wind velocity was 7 knots and the wind direction was 310 degrees. The pilot reported while practicing take offs and landings, he made a standard approach and landing to runway 35. On takeoff, he reduced the flaps to zero degrees and he reported that the airplane was under control and over the runway centerline. After he applied full power and right rudder before lifting off the ground, the airplane started turning to the left sharply. He applied additional right rudder, he reduced the power, and applied full brakes. The airplane departed the runway to left into a swamp and nosed over. The airplane sustained substantial damage to the right wing and the firewall. The pilot verified that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot reported that the wind velocity at the accident site was 6 to 7 knots and the wind direction was 330 degrees. The weather reporting facility at the accident site reported that about 3 minutes after the accident time that the wind velocity was 7 knots and the wind direction was 310 degrees. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2016_GAA16CA181.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (icing, runway excursion). 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.
- arXiv 2026 · arXiv preprint Enabling Beyond-Visual-Line-of-Sight Drones Operation over Open RAN 5G Networks with Slicing
Among the foretold claims of the transition from 5G to 6G, Beyond-Visual-Line-of-Sight (BVLoS) drone operation has emerged as a prominent Internet-of-Robots enabler.
- NASA NTRS 2026 · Contractor Report (CR) Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…