NTSB CAROL · Event
Event ATL93FA025
Aircraft involved
Probable cause & findings
THE PILOT FAILED TO EVALUATE THE WIND CONDITIONS AND TOOK OFF WITH A TAILWIND WHICH RESULTED IN THE COLLISION WITH A TREE ON THE DEPARTURE END OF THE RUNWAY. FACTORS WERE DARK NIGHT AND TAILWIND.
Factual narrative
THE NEWLY CERTIFICATED PILOT ATTEMPTED A VISUAL NIGHT TAKEOFF WITH A TAILWIND. THE FLIGHT WAS OBSERVED AS IT CLIMBED OUT FROM RUNWAY 27 AND COLLIDED WITH A TREE ABOUT 1/4 MILE FROM THE END OF THE SOD RUNWAY. AFTER COLLIDING WITH THE TREE, THE AIRPLANE CONTINUED ABOUT 200 PLUS FEET BEFORE IMPACTING THE GROUND INVERTED. WRECKAGE EXAMINATION FAILED TO DISCLOSE A MECHANICAL MALFUNCTION OR COMPONENT FAILURE. HOWEVER, THE CARBURETOR EXAMINATION REVEALED THAT A COMPOSITE MATERIAL TYPE FLOAT WAS INSTALLED. THE AIRPLANE WAS SERVICED WITH 30 GALLONS OF AUTOMOTIVE FUEL. ADDITIONALLY ACCORDING TO THE OPERATOR'S MANUAL, THERE IS NO PERFORMANCE DATA AVAILABLE TO THE PILOT FOR A TAILWIND TAKEOFF. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_ATL93FA025.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 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.
- 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…
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