NTSB CAROL · Event
Event ATL86FA227
Registry · N5299J
FAA Aircraft Registry record.
Make / Model
AEROSTAR INTERNATIONAL INC RX 8
Year of manufacture
2001
Engine
NONE NONE
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20010920
ADS-B equipped
Yes — Mode-S A6ADF9
Registrant of record
OLIN MICHAEL A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
DURING A NORMAL TAKEOFF THE PILOT EXPERIENCED A DUAL ENGINE FAILURE ABOUT 10 FEET ABOVE THE RUNWAY. THE PILOT STATED THAT HE LANDED ON THE REMAINING RUNWAY AND ATTEMPTED AN 80 DEGREE LEFT TURN ONTO TAXIWAY 'C'. THE AIRCRAFT FAILED TO NEGOTIATE THE TURN AT THE ROLLOUT SPEED AND ROLLED DOWN A RAVINE WHERE THE IT COLLIDED WITH A TREE. THE INVESTIGATION FAILED TO DETERMINE A MECHANICAL MALFUNCTION OR FAILURE DURING THE POST CRASH EXAMINATION. BOTH ENGINES OPERATED NORMALLY WITH THE EXISTING AIRCRAFT SYSTEMS AND FUEL ON BOARD. IT WAS ALSO DETERMINED THAT THE PILOT HAD AMPLE RUNWAY AND GRASSY AREAS AVAILABLE TO SUCCESSFULLY COMPLETE AN EMERGENCY ROLLOUT. BOTH PILOTS WERE CERTIFICATED TO OPERATE THE AIRCRAFT; HOWEVER, THE PILOT IN THE LEFT SEAT WAS NOT INSTRUMENT RATED. THE FLIGHT WAS DEPARTING UNDER INSTRUMENT FLIGHT RULES. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1986_ATL86FA227.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 ↗