NTSB CAROL · Event
Event ATL83FA178
Aircraft involved
Factual narrative
THE ACFT CRASHED IN A WOODED AREA AFTER A TOUCH AND GO LANDING. THE WING FLAPS LEVER HAD BEEN PLACED TO THE UP POSITION BUT THE FLAPS DID NOT RETRACT. WHEN THE CFI FINALLY NOTICED THAT THE FLAPS WERE NOT UP HE TOOK OVER AT ABOUT 200 FT AGL AND STARTED A SHALLOW RIGHT TURN. THE AIRSPEED WAS ABOUT 62 MPH INDICATED WHEN THE CFI TURNED LEFT WITH A NOSE HIGH ATTITUDE. THE ACFT STALLED AND SPUN TO THE GROUND ABOUT 600 FT FROM THE DEPARTURE END OF THE RWY. THE FLAP INDICATOR REGISTERED 33 DEGREES. THERE WAS A NOTICE POSTED BELOW THE FLAP INDICATOR WHICH READ 'USE 30 DEGREE FLAP MAX'. INVESTIGATION REVEALED THAT THE FLAP MOTOR FUSE WAS BLOWN. BOTH PLTS HAD BEEN RESTRAINED BY SHOULDER HARNESS SECURED THROUGH INTERIOR PLASTIC MOLDING. AT IMPACT THEY CAME LOOSE. THIS ACFT WAS NOT MANUFACTURED WITH SHOULDER HARNESS. ACFT LOGS DID NOT SHOW WHERE, WHEN OR BY WHOM THE EXISTING HARNESS WAS INSTALLED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1983_ATL83FA178.txt.
Findings + structured fields enriched from FAA avall.mdb.
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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 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…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- arXiv 2021 · arXiv preprint
Investigation of flow field of clap & fling motion using immersed boundary coupled lattice Boltzmann method
This paper deals with the investigation of flow field due to clap and fling mechanism using immersed boundary coupled with lattice Boltzmann method.
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