NTSB CAROL · Event
Event ATL89LA156
Registry · N1652G
FAA Aircraft Registry record.
Make / Model
CHAMPION 7GCBC
Year of manufacture
1968 · 21 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19680912
ADS-B equipped
Yes — Mode-S A106E6
Registrant of record
RUNWAY 5 LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE IMPROPER INSTALLATION/MODIFICATION OF THE BANNER TOW SYSTEM, WHICH JAMMED THE RUDDER DURING A LANDING. THE WIND AND TERRAIN CONDITIONS WERE RELATED FACTORS.
Factual narrative
AFTER DROPPING A BANNER, THE PLT ELECTED TO MAKE A 3-POINT LNDG AT A SMALL PVT ARPT WITH THE WND GUSTING TO 15 KTS. HE RPRTD THAT JUST BEFORE TOUCHDOWN, THE ACFT ENCTRD A DOWNDRAFT & HE INCREASED BACK PRESSURE ON THE CONTROL STICK TO BREAK THE DESCENT. THE ACFT CONTACTED THE RWY TAIL 1ST & BOUNCED SLIGHTLY. IT THEN SWERVED TO THE LEFT, WENT OFF THE RWY & NOSED OVER IN AN ADJACENT BEAN FIELD. AN EXAM OF THE ACFT REVEALED THE RUDDER HAD CONTACTED ONE OF THE BANNER TOW HOOKS & WAS JAMMED TO THE LEFT. THE BANNER TOW INSTALLATION HAD RECENTLY BEEN MODIFIED FROM A SINGLE HOOK TO A MULTIPLE HOOK SYS. IN A LETTER DATED 5/31/89, THE FAA NOTIFIED THE FACILITY WHICH PERFORMED THE MODIFICATION THAT THE MULTIPLE HOOK INSTALLATION COULD NOT BE APPROVED AS SUBMITTED (ON FAA FORM 337). Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1989_ATL89LA156.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 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…
- 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…
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