ATL90FA158
1990-08-11 · LOCUST GROVE, Georgia, United States · Fatal · 1 aircraft · Status: Completed
Airport GA04
Current FAA registration · N9871C
- Make / Model
- NORTH AMERICAN T-6G
- Year of manufacture
- 1949 · 41 years old at event
- Engine
- P&W R1340 SERIES (600 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19590203
- ADS-B equipped
- Yes — Mode-S ADC7A3
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN AIRCRAFT CONTROL DURING MANEUVERING FLIGHT, ALLOWING THE AIRPLANE TO STALL WITHOUT SUFFICIENT ALTITUDE FOR RECOVERY.
Factual narrative
SHORTLY AFTER TAKEOFF, WITNESSES REPORTED THAT THE AIRPLANE ENTERED A STEEP, NOSE HIGH, LEFT TURN. ONE WITNESS STATED THAT HE (THE PILOT) 'HONKED IT UP' AND 'REALLY YANKED IT BACK'. WHEN THE AIRPLANE WAS ABOUT 300 TO 400 FEET AGL, THE WINGS LEVELED, 'WAGGED', AND THE AIRPLANE THEN ROLLED INTO THE TERRAIN IN A STEEP, NOSE LOW ATTITUDE. REPORTEDLY, THE AIRPLANE HAD BEEN TOPPED WITH FUEL PRIOR TO TAKEOFF. ALL WITNESSES STATED THAT THE ENGINE WAS RUNNING ALL THE WAY TO GROUND IMPACT. AN EXAMINATION OF THE WRECKAGE DID NOT REVEAL EVIDENCE OF MECHANICAL MALFUNCTION OR FAILURE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_ATL90FA158.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 or causal vocabulary (stall). All research papers
- 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 …
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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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…