NTSB CAROL · Event
Event ATL88LA024
Registry · N11GL
FAA Aircraft Registry record.
Make / Model
ZOAR CUBS LLC CCX-2300
Year of manufacture
2022
Engine
LYCOMING IO-390 SER (210 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20221118
ADS-B equipped
Yes — Mode-S A02A7B
Registrant of record
XCUBAIR LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
PIC RPTED REAR ENG QUIT AFTER TAKE-OFF. FUEL SELECTOR FOUND ON RIGHT MAIN TANK WHICH WAS EMPTY. PROP WAS NOT FEATHERED AND LANDING GEAR WAS FOUND IN TRANSIENT POSITION AFTER CRASH. OWNERS MANUAL CAUTIONS AGAINST HIGHER DRAG WITH GEAR IN TRANSIT DUE TO LARGE GEAR DOORS AND LESS SINGLE ENGINE CAPABILITY WITH FRONT ENGINE. PIC STARTED TURN BACK TO ARPT IMMEDIATELY AFTER ENGINE FAILURE. MINIMAL SINGLE ENGINE CAPABILITY WAS FURTHER DEGRADED BY NON-PERFORMANCE OF EMERGENCY PROCEDURE, PREMATURE MANEUVERING, AND DELAYED GEAR RETRACTION. THE ACFT WAS NOT ABLE TO MAINTAIN ALTITUDE AND, AFTER UNSUCCESSFULLY ATTEMPTING TO RESTART THE REAR ENGINE, THE PLT SELECTED A FORCED LANDING AREA. ON FINAL, POWER LINES WERE OBSERVED AND IN AN EFFORT TO AVOID THEM, TWO UTILITY POLES WERE STRUCK. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1987_ATL88LA024.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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…
Browse the full corpus — academia portal ↗