NTSB CAROL · Event
Event ATL02LA009
Registry · N117JB
FAA Aircraft Registry record.
Make / Model
CESSNA 172N
Year of manufacture
1978 · 23 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19780322
ADS-B equipped
Yes — Mode-S A046FE
Registrant of record
GENERATIONS FLYING CLUB LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed during a low-altitude aerobatic maneuver, which resulted in an inadvertent stall/spin and subsequent uncontrolled descent into terrain.
Factual narrative
On November 3, 2001, at 1310 eastern standard time, a James E. Bass, Moni Motor Glider, N117JB, collided with the ground while maneuvering at Mallard's Landing, a private airstrip, in Locust Grove, Georgia. The aircraft was owned and operated by the pilot, and the personal flight was conducted under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage, and the airline transport pilot received fatal injuries. The local flight departed Locust Grove, Georgia, at an undetermined time. The aircraft and several others were participating in a fly-in at Mallard's Landing. According to witnesses, the aircraft executed a high-powered pass approximately 25 feet above ground level down runway 07, then performed an abrupt pull-up into steep climbing loop maneuver. About 200 to 300 feet above the ground, the aircraft was inverted at the top of the loop, then it rolled upright and entered what appeared to be a stall, followed by a spin, and collided with the ground in an 80-degree nose-low attitude. Two witnesses reported the engine "burped," while other witnesses reported the engine sounded as if it were running smoothly. Examination of the accident site revealed wreckage debris was scattered over an area approximately 40 feet square in the back yard of a residence adjacent to the sod runway. Debris from the propeller spinner and cowling was embedded in the ground, and the propeller assembly was separated and found 30 feet from the main wreckage. The nose section was separated, and the wings displayed extensive perpendicular crush damage from the leading edge aft. Continuity was established from the cockpit controls to the flight control surfaces. Engine continuity was established and both cylinders exhibited compression when the engine was turned by hand. The carburetor was destroyed. The Operator's Manual for the Rotax 447 engine states on Page 4-3, "This engine is not suitable for acrobatics (inverted flight, etc.)," and on Page 4-2, "Never fly the aircraft equipped with this engine at locations, airspeeds, altitudes, or other circumstances from which a successful no-power landing cannot be made after sudden engine stoppage." The postmortem examination of the pilot was performed on November 4, 2001, by Dr. John B. Parker at the Henry County Medical Center Morgue in Stockbridge, Georgia. Blount force trauma The Forensic toxicology was performed by the FAA Toxicology and Accident Laboratory, Oklahoma City, Oklahoma. The tests were negative for carbon monoxide, cyanide, drugs and alcohol. The aircraft maintenance logbooks were not recovered for examination. The aircraft executed a high-powered pass approximately 25 feet above ground level down runway 07, then performed an abrupt pull-up into steep climbing loop maneuver. About 200 to 300 feet above the ground, the aircraft was inverted at the top of the loop, then it rolled upright and entered what appeared to be a stall, followed by a spin, and collided with the ground. Two witnesses reported the engine "burped," while other witnesses reported the engine sounded as if it were running smoothly. Examination of the wreckage revealed the nose section was separated, and the wings displayed extensive perpendicular crush damage. Continuity was established from the cockpit controls to the flight control surfaces. Engine continuity was established and both cylinders exhibited compression when the engine was turned by hand. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_ATL02LA009.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, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2018 · Article (Volume 6: Ceramics; Controls, Diagnostics, and Instrumentation; Education; Manufacturing Materials and Metallurgy)
Fleet Monitoring and Diagnostics Framework Based on Digital Twin of Aero-Engines
Monitoring aircraft performance in a fleet is fundamental to ensure optimal operation and promptly detect anomalies that can increase fuel consumption or compromise flight safety.
- arXiv 2026 · arXiv preprint
On the Value of Base Station Motion Knowledge for Goal-Oriented Remote Monitoring with Energy-Harvesting Sensors
This paper investigates goal-oriented remote monitoring of an unobservable Markov source using energy-harvesting sensors that communicate with a mobile receiver, such as a Low Earth Orbit (LEO) satell…
- arXiv 2026 · arXiv preprint
Close-enough general routing problem for multiple unmanned aerial vehicles in monitoring missions
In this paper, we introduce a close-enough multi-UAV general routing problem (CEMUAVGRP) where a fleet of homogeneous UAVs conduct monitoring tasks containing nodes, each of which has its disk neighbo…
- arXiv 2025 · arXiv preprint
Safe Path Planning and Observation Quality Enhancement Strategy for Unmanned Aerial Vehicles in Water Quality Monitoring Tasks
Unmanned Aerial Vehicle (UAV) spectral remote sensing technology is widely used in water quality monitoring. However, in dynamic environments, varying illumination conditions, such as shadows and spec…
- arXiv 2025 · arXiv preprint
Multi-UAV Flood Monitoring via CVT with Gaussian Mixture of Density Functions for Coverage Control
This study presents a control strategy for coordinating multiple unmanned aerial vehicles (UAVs) to monitor unknown flood regions and estimate the extent of inundation.
- arXiv 2025 · arXiv preprint
Task Allocation of UAVs for Monitoring Missions via Hardware-in-the-Loop Simulation and Experimental Validation
This study addresses the optimisation of task allocation for Unmanned Aerial Vehicles (UAVs) within industrial monitoring missions.
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