ATL89DMG06
1989-08-11 · HENDERSONVILLE, North Carolina, United States · Fatal · 1 aircraft · Status: Completed
Airport 0A7
Aircraft involved
Probable cause & findings
ENGINE FAILURE DUE TO CARBURETOR ICE.
Factual narrative
THE HOMEBUILT AIRCRAFT COLLIDED WITH A HANGER WHILE ON FINAL APPROACH TO LAND AFTER A LOSS OF POWER. THE TEMP/DEW POINT RATIO WAS 76/55. THIS WAS A DEMONSTRATION FLT WHICH FOLLOWED A SOLO, CHECK OUT FLIGHT AROUND THE PATTERN AND TWO OTHER DEMONSTRATION FLIGHTS. ON-SITE EXAMINATION REVEALED THE PRESENCE OF FUEL AND THAT THE PROPELLER WAS TURNING AT IMPACT. THE DAMAGED PROPELLER AND CARBURETOR WERE REPLACED BECAUSE THE MOUNT FOR THE CARBURETOR WAS BENT, THE GAP AROUND THE CARBURETOR AND FLANG WAS SEALED WITH A SILICONE SEALER AND THE ENGINE RAN SMOOTHLY DURING A TEST RUN. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1989_ATL89DMG06.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
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…