NTSB CAROL · Event
Event ATL82DA138
Aircraft involved
Factual narrative
ABOUT EIGHT MINUTES AFTER TAKEOFF, THE PILOT DECLARED AN EMERGENCY AND REPORTED AN ENGINE FAILURE. HE DIVERTED, BUT WAS UNABLE TO REACH THE AIRPORT. A GEAR-UP LANDING WAS MADE ABOUT ONE MILE SHORT OF THE RUNWAY. AN EXAMINATION OF THE AIRCRAFT REVEALED THAT THE VACUUM PUMP WAS NOT INSTALLED ON THE ENGINE AND THERE WAS NO COVER PLATE OVER THE OPENING. OIL WAS OBSERVED ALONG THE RIGHT SIDE OF THE FUSELAGE. THE PILOT STATED THAT A MECHANIC, WHO HAD REMOVED THE VACUUM PUMP, HAD ADVISED THAT THERE WOULD BE NO PROBLEMS WITH FLYING THE AIRCRAFT WITHOUT THE PUMP. A TEARDOWN EXAMINATION REVEALED THAT THE NO. 4 CONNECTING ROD HAD FAILED. THE NO. 2 AND 3 CONNECTING ROD BEARINGS WERE BURNT OUT. THE NO. 5 AND 6 ROD BEARINGS WERE BADLY SCORED. THE ENGINE OIL PUMP WAS INTACT AND CONTAINED RESIDUAL OIL; THE PUMP GEARS APPEARED NORMAL. ABOUT 1 1/2 QUARTS OF OIL WAS FOUND IN THE ENGINE BEFORE DISASSEMBLY. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1982_ATL82DA138.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 (stall, 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.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
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