NTSB CAROL · Event
Event ATL87FA123
Aircraft involved
Factual narrative
THE RIGHT ENGINE FAILED DURING TAKEOFF IMMEDIATELY AFTER ROTATION 3000' DOWN THE 7,002' RWY 16. THE PLT CONTINUED THE FLT AND THE LANDING GEAR REMAINED EXTENDED. THE UNAUTHORIZED PLT RATED PAX MADE XMISSIONS TO THE TOWER. WITNESSES RPTED THAT THE ACFT REACHED APPROX. 150' THEN DESCENDED INTO TREES 20 DEGREES TO THE RIGHT OF RWY CENTERLINE AND 3,000' SOUTH OF THE ARPT. THE PRE- 1979 3RD STAGE STATOR ASSY IN THE RIGHT ENGINE DID NOT HAVE THE LATEST MANUFACTURE WELDING PROCESS/INSPECTION AND FAILED CAUSING THE UNCONTAINED TURBINE FAILURE. INSTRUMENTS IN THE WRECKAGE INDICATED THAT AN UNDETERMINABLE LOSS OF ELECTRICAL POWER OCCURRED AT THE TIME OF ENGINE FAILURE. PERFORMANCE DATA INDICATED THAT A SAFE LANDING COULD HAVE BEEN MADE ON THE REMAINING RWY PAST THE POINT OF ENGINE FAILURE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1987_ATL87FA123.txt.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). 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
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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