NTSB CAROL · Event
Event ATL93LA019
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO FOLLOW INSTRUMENT PROCEDURES WHILE CONDUCTING AN INSTRUMENT APPROACH WHICH RESULTED IN THE COLLISION WITH TREES; THE PILOT DESCENDED BELOW THE MINIMUM DESCENT ALTITUDE.
Factual narrative
THE PILOT RECEIVED A WEATHER BRIEFING AND FILED AN INSTRUMENT FLIGHT PLAN TO THE DESTINATION AIRPORT WITHOUT LISTING AN ALTERNATE AIRPORT. UPON ARRIVING AT HIS PLANNED DESTINATION, HE EXECUTED TWO INSTRUMENT APPROACHES AND WAS UNABLE TO ESTABLISH VISUAL CONTACT WITH THE GROUND. HE REQUESTED A THIRD APPROACH FROM AIR TRAFFIC CONTROL AND COLLIDED WITH TREES ABOUT THREE MILES SHORT OF THE AIRPORT WHILE ON FINAL APPROACH. EXAMINATION OF THE AIRPLANE FAILED TO DISCLOSE A MECHANICAL MALFUNCTION OR A COMPONENT FAILURE. ACCORDING TO THE PUBLISHED APPROACH PROCEDURE THE MINIMUM DESCENT ALTITUDE IS 800 FEET MSL; THE PILOT DESCENDED BELOW THE PUBLISHED MINIMUMS. THE PILOT DID NOT REPORT A PROBLEM WITH THE AIRPLANE OR THE ONBOARD FLIGHT INSTRUMENTS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_ATL93LA019.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. 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 2011 · Conference Paper
Joint thunderstorm operations using the NASA F-106B and FAATC/AFWAL Convair 580 airplanes
During the 1985 thunderstorm season, three joint thunderstorm research flights were conducted within 100 n.mi. of NASA Langley by the NASA Storm Hazards F-106B and the FAA/USAF CV-580 research airplan…
- NTSB Aircraft Accident Reports 2004 · Accident report
In-Flight Separation of Vertical Stabilizer — American Airlines Flight 587
American Airlines 587 (A300-605R) Belle Harbor, NY, November 12, 2001 — 265 fatalities. Investigation of the post-takeoff in-flight breakup of American 587 over Belle Harbor.
- NASA NTRS 2024 · Presentation
American Airlines Flight 587 Crash Investigation: NASA Langley Research Center Participation and Perspective
- NASA NTRS 2019 · Other
Documentation for Three Wake Vortex Model Data Sets from Simulation of Flight 587 Wake Vortex Encounter Accident Case
This document contains a general description for data sets of a wake vortex system in a turbulent environment. The turbulence and thermal stratification of the environment are representative of the co…
- NASA NTRS 2016 · Conference Paper
An overview of SAE ARP 1587: Aircraft gas turbine engine monitoring system guide
A systematic approach to developing an engine monitoring system (EMS) is outlined. An extensive shopping list of EMS capabilities and benefits are included.
- arXiv 2025 · arXiv preprint
Numerical Investigation of Discontinuous Ice Effects on Swept Wings
This study investigates the aerodynamic performance and flow structures of infinite swept wings with artificially simulated discontinuous ice using an enhanced delayed detached-eddy simulation.
Browse the full corpus — academia portal ↗