NTSB CAROL · Event
Event ATL96LA004
Registry · N102JL
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SF50
Year of manufacture
2020
Engine
WILLIAMS FJ33-5A
Seats / Engines
7 seats · 1 engine
Last airworthiness date
20200321
ADS-B equipped
Yes — Mode-S A00CF5
Registrant of record
3D ENTERPRISES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the noninstrument-rated pilot's intentional VFR flight into instrument meteorological conditions which led to a loss of control.
Factual narrative
HISTORY OF FLIGHT
On October 13, 1995, at 1605 eastern daylight time, a Lopez Lancair 360, N102JL was destroyed following an in-flight breakup near Atlanta, Georgia. The non-instrument rated private pilot was fatally injured in the accident. The aircraft was being operated under the provisions of 14 CFR Part 91 by the pilot. Instrument meteorological conditions existed at the time of the accident, and an instrument flight rules flight plan had been filed for the flight. The flight departed Runway 20 at the Dekalb-Peachtree Airport at 1554, and was destined for Boca Raton, Florida. The non-instrument rated private pilot filed and received an instrument rules flight plan from Atlanta, Georgia to Boca Raton, Florida. Transcripts of radio communications between the pilot and Air Traffic Control (ATC) personnel show that, shortly after takeoff, the pilot reported having problems with one of the aircraft gyro's. The pilot later reported that the gyro problem had corrected itself, but the radio transcript shows that the pilot continued to have difficulty in maintaining heading and altitude assignments. The aircraft was last observed on radar at an altitude of 4,400 feet above mean sea level, and then disappeared off the radar screen. Witnesses, in the accident area, stated they heard a loud bang, and that the aircraft appeared to break-up just prior to impacting the terrain.
PERSONNEL INFORMATION
The pilot held a private pilot certificate with airplane single engine, multiengine, and helicopter ratings. The Federal Aviation Administration has no record that the pilot had ever held an instrument rating. He held a second class medical certificate issued in May of 1995, with no restrictions. No record of the pilot's flight time could be located. Additional personnel information may be obtained on page 4 of this report under section titled First Pilot Information.
AIRCRAFT INFORMATION
The Lopez Lancair 360 is a homebuilt, low wing, retractable tricycle gear airplane. The aircraft was constructed entirely of composite materials. The airplane was built by Mr. Jorge Lopez, and Federal Aviation Administration (FAA) aircraft records show Mr. Lopez as the registered owner of the aircraft. No maintenance records on the aircraft could be located. Additional aircraft information may be found on page 2 of this report under section titled Aircraft Information.
METEOROLOGICAL INFORMATION
Instrument meteorological conditions existed at the time of the accident. Additional meteorological information may be obtained on page 4 of this report under section titled Weather Information.
WRECKAGE AND IMPACT INFORMATION
The aircraft wreckage was distributed over a wooded residential area. The wreckage distribution path was approximately 2,500 feet in length, on a heading of approximately 180 degrees. The first pieces of the wreckage found in the wreckage path were the left and right wings. The leading edges of the wings did not show any signs of impact with the trees. The fuselage was located about mid point of the wreckage site, and the engine was located about 2,500 feet in the direction of distribution from the beginning of the wreckage distribution path.
MEDICAL AND PATHOLOGICAL INFORMATION
An autopsy of the pilot was performed by Dr. Steven F. Dunton of the Fulton County Medical Examiners Office. The autopsy report lists the cause of death as generalized trauma. A toxicological examination of the pilot was performed by the Federal Aviation Administration Accident and Research Laboratory in Oklahoma City, Oklahoma. Dr. Soper stated that the examination results were negative for the use of ethanol, and drugs. The noninstrument-rated pilot filed for and received an instrument flight plan clearance from Atlanta to Boca Raton, Florida. The weather at the time of the accident was IMC. Transcripts of radio communications indicated that the pilot was having problems maintaining altitude and heading. Shortly after departure the pilot reported that he thought that one of the aircraft gyros was not operating properly. He later reported that he believed the problem had corrected itself. Witnesses observed the aircraft descend out of the base of the clouds and break up in flight. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_ATL96LA004.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 (loss of control, imc, 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.
- arXiv 2022 · arXiv preprint
Zero Touch Coordinated UAV Network Formation for 360° Views of a Moving Ground Target in Remote VR Applications
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- NASA NTRS 2019 · Other
Differential Pressures on a Pitot-venturi and a Pitot-static Nozzle over 360 Degrees Pitch and Yaw
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- NTSB Aircraft Accident Reports 2002 · Accident report
Loss of Control and Impact with Pacific Ocean — Alaska 261
Alaska Airlines Flight 261 (MD-83) Pacific Ocean, January 31, 2000 — 88 fatalities. Definitive investigation of the Alaska 261 pitch-runaway-and-loss-of-control crash.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- Semantic Scholar 2025 · Article (Applied Sciences)
Decision-Making Framework for Aviation Safety in Predictive Maintenance Strategies
The implementation of predictive maintenance (PM) in aviation presents unique challenges due to strict safety requirements, complex operational environments, and regulatory constraints.
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