MKC88LA114
1988-06-21 · ELDON, Missouri, United States · Serious · 1 aircraft · Status: Completed
Airport H79
Aircraft involved
Probable cause & findings
TOTAL FAILURE OF THE POWERPLANT DUE TO AN OIL LINE RUPTURE, AND PROPER TOUCHDOWN POINT NOT ATTAINED BY THE PILOT IN COMMAND.
Factual narrative
DURING A BUSINESS, CROSS-COUNTRY FLIGHT, THE PRIVATE PILOT SAID THAT HE HEARD A POPPING NOISE FOLLOWED BY OIL APPEARING ON THE WINDSHEILD. SHORTLY AFTER THE ENGINE BEGAN TO LOSE POWER, THEN QUIT. AN EMERGENCY LDG WAS ATTEMPTED ON AN AIRPORT, BUT THE ACFT LANDED SHORT OF THE RUNWAY, STRUCK A FENCE AND COLLIDED WITH THE TERRAIN. THE ACFT CAME TO REST ABOUT 25 FEET FROM THE RUNWAY. POST ACCIDENT INVESTIGATION REVEALED A BROKEN ENGINE OIL LINE WHICH RESULTED IN LOSS OF ENGINE OIL AND SUBSEQUENT TOTAL ENGINE FAILURE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1988_MKC88LA114.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- arXiv 2022 · arXiv preprint Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
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- 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…