NTSB CAROL · Event
Event ENG13WA003
Aircraft involved
Factual narrative
On October 20, 2012, a Boeing 737-800, registered JA342J, operated by JAL Express, departed from Tokyo International Airport and declared an emergency No. 1 engine failure during climb. The pilot reported low engine RPM and high exhaust gas temperature warnings. Flight crew operating manual procedures were followed and the No. 1 engine was shutdown before the aircraft returned to Tokyo International Airport for an uneventful single engine landing. No injuries were reported to the 144 passengers and crew members on board. Damage to the high pressure compressor and turbine blades was noted during a preliminary inspection by ground crews. The Japan Transport Safety Board (JTSB) is investigating the incident. The NTSB has was notified of the incident under the provisions of Annex 13 to the Convention of Civil Aviation as the state of manufacture and design for multiple components on the CFM56-7B engine. All inquiries concerning this incident should be directed to the JTSB at: Director-General Secretariat of the Aircraft and Railway Accidents Investigation Commission Ministry of Land, Infrastructure and Transport 2-1-2, Kasumigaseki, Chiyoda-ku Tokyo 100-8918 Japan Tel.: (81) 3 5253 8813 E-mail: [email protected] Fax: (81) 3 5253 1677 AFTN: RJTDYAYA Cable: KOKUKYOKU-TOKYO Website: http://www.motnet.go.jp/araic/index.html Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2012_ENG13WA003.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…
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