NTSB CAROL · Event
Event ATL84FA116
Registry · N9011P
FAA Aircraft Registry record.
Make / Model
AIRBUS A319-115
Year of manufacture
2013
TCDS
A28NM · AIRBUS SAS
Engine
CFM INTL CFM56-5B6
Seats / Engines
147 seats · 2 engines
Last airworthiness date
20131029
ADS-B equipped
Yes — Mode-S AC756C
Registrant of record
WILMINGTON TRUST CO TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE ACCIDENT OCCURRED ON MISSED APPROACH AT NIGHT IN WEATHER CONDITIONS BELOW THE DESTINATION MINIMUMS AFTER APRX 5 HOURS AND 25 MINUTES OF FLIGHT. PERFORMANCE COMPUTATIONS INDICATED THE ACCIDENT OCCURRED AT OR NEAR THE TIME OF PROJECTED FUEL EXHAUSTION. METALLURGICAL EXAMINATION COULD NOT DETERMINE THAT A MALFUNCTION IN THE ALTIMETER OCCURRED BEFORE IMPACT. SEVERAL WITNESSES HEARD THE ENGINE 'CUT-OUT' BEFORE IMPACT. IT WAS DETERMINED THAT THE ACCIDENT OCCURRED DURING AN UNCONTROLLED DESCENT IN INSTRUMENT CONDITIONS AFTER AN ENGINE FAILURE AS A RESULT OF FUEL EXHAUSTION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1984_ATL84FA116.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 (fuel exhaustion, 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 ↗