NTSB CAROL · Event
Event ATL87LA140
Aircraft involved
Factual narrative
THE PLT REPORTED THAT HE CLOSED THE THROTTLE TO SIMULATE AN ENGINE FAILURE AFTER TAKEOFF FROM RWY 06, AT ABOUT 400-500 FT AGL. HE SUBSEQUENTLY MADE A 180 DEGREE TURN BACK TOWARD THE ARPT TO PRACTICE A SIMULATED FORCED LDG, AND THE ACFT SINK RATE INCREASED TO A GREATER RATE THAN 'EXPECTED'. HE THEN ADDED FULL THROTTLE, BUT THE ENGINE DID NOT RESPOND. THE ACFT IMPACTED GRASSY TERRAIN SHORT OF AND TO THE RIGHT OF THE RWY, AND SLID ABOUT 130 FEET. A POST-CRASH FIRE ENSUED. THE PLT STATED THAT HE HAD 11 TOTAL FLT HRS IN THIS MAKE AND MODEL, ALL OF WHICH WERE OBTAINED IN THIS ACFT. HE NOTED THAT THE ACFT HAD SAT UNUSED FOR THREE YEARS PRIOR TO HIS PURCHASING IT, AND THAT IT HAD RECEIVED AN ANNUAL INSPECTION A WEEK PRIOR TO THE ACCIDENT. THE ENGINE CARBURETOR WAS REPORTEDLY EQUIPPED WITH A 'LEATHER-SKIRT' TYPE ACCELERATOR PUMP. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1987_ATL87LA140.txt.
Findings + structured fields enriched from FAA avall.mdb.
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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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