BOEING 787 near Boston, MA — 2013-01-07
- Date
- 2013-01-07
- Location
- Boston, MA, USA
- Airport
- BOS
- Aircraft
- BOEING 787
- Registration
- JA829J
- Category
- Airplane
- Fatalities
- 0
Probable cause
an internal short circuit within a cell of the auxiliary power unit (APU) lithium-ion battery, which led to thermal runaway that cascaded to adjacent cells, resulting in the release of smoke and fire. The incident resulted from Boeing's failure to incorporate design requirements to mitigate the most severe effects of an internal short circuit within an APU battery cell and the Federal Aviation Administration's failure to identify this design deficiency during the type design certification process.
NTSB narrative
The Safety Board's full report is available at http://www.ntsb.gov/investigations/AccidentReports/Pages/aviation.aspx. The Aircraft Accident Report number is NTSB/AAR-14/01. On January 7, 2013, about 1021 eastern standard time, smoke was discovered by cleaning personnel in the aft cabin of a Japan Airlines (JAL) Boeing 787-8, JA829J, which was parked at a gate at General Edward Lawrence Logan International Airport (BOS), Boston, Massachusetts. About the same time, a maintenance manager in the cockpit observed that the auxiliary power unit (APU) had automatically shut down. Shortly afterward, a mechanic opened the aft electronic equipment bay and found heavy smoke coming from the lid of the APU battery case and a fire with two distinct flames at the electrical connector on the front of the case. None of the 183 passengers and 11 crewmembers were aboard the airplane at the time, and none of the maintenance or cleaning personnel aboard the airplane was injured. Aircraft rescue and firefighting personnel responded, and one firefighter received minor injuries. The airplane had arrived from Narita International Airport, Narita, Japan, as a regularly scheduled passenger flight operated as JAL flight 008 and conducted under the provisions of 14 Code of Federal Regulations (CFR) Part 129.
NTSB coding
- Fire/smoke (non-impact) · Other
Evidence available
- CVR
- Video
- FDR / data
- 104 docket documents
Docket documentsshowing 50 of 104
- Cockpit Voice Recorder 12 - Specialist Summary Report of Investigationcvr
- Flight Data Recorder 10 - Attachment 1: Tabular Data From Forward EAFRfdr
- Flight Data Recorder 10 - Attachment 2: Tabular Data From Aft EAFRfdr
- Flight Data Recorder 10 - Factual Report of Group Chairmanfdr
- Flight Data Recorder 10 - Factual Report of Group Chairman - Addendum 1fdr
- Flight Data Recorder 10 - Factual Report of Group Chairman - Addendum 1 - Attachment 1fdr
- Airworthiness 17E – Example of Lithium Ion Battery Information Available on the Internet from www.batteryuniversity.com, Author: Isidor Buchmannform
- Airworthiness 17H – Excerpts from Thales BCU Q2 Qualification Test Procedure, Electrical Performanceform
- Retention / Release of Wreckage Formform
- Airports/ARFF 16 - Attachment 4: BOS ARFF Interviewsinterview
- Airports/ARFF 16 - Attachment 6: JAL Mechanic Statementinterview
- Pilot Statementinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statement - Station Managerinterview
- Witness Statement - Turn Around Coordinatorinterview
- Airports/ARFF 16 - Attachment 1: BOS Airport Diagramother
- Airports/ARFF 16 - Attachment 2: BOS ARFF Fire Alarm Logother
- Airports/ARFF 16 - Attachment 5: BOS ARFF Response Routeother
- Airports/ARFF 16 - Attachment 7: BOS ARFF Boeing 787 Familiarization Training Recordsother
- Airports/ARFF 16 - Attachment 8: Boeing Emergency Response Diagrams for Li-ion Batteryother
- Airworthiness - UL Analysis of Asset 459 Cell 5other
- Airworthiness - UL Battery Nail Penetration Test 15C Groundedother
- Airworthiness - UL Battery Nail Penetration Test 70C Ungroundedother
- Airworthiness 17A – Excerpts from Boeing Battery Specification Control Drawingother
- Airworthiness 17B – Special Conditions: Airbus Model A380-800 Airplane, Lithium Ion Battery Installationother
- Airworthiness 17D – Excerpts from Boeing Battery Charger Unit (BCU) Specification Control Drawingother
- Airworthiness 17F – Boeing Provided Presentation about Battery Smoke and Venting at Hamilton Sundstrand Airplane Power Systems Integration Facility (APSIF)other
- Airworthiness 17G – Thermal Environment section from Thales/GS-Yuasa Interface Control Documentother
- Airworthiness Directive 2013-2-51other
- Designation of Chairman of Board of Inquiry 1Bother
- Designation of Hearing Officer 1Cother
- Designation of Parties to Hearing 1Dother
- Emergency Airworthiness Directive 2013-02-51other
- Investigative Hearing Exhibit List 1Fother
- Investigative Hearing Witness List 1Gother
- Investigative Hearing Witness Professional Biographies 1Hother
- Materials 15A – Excerpts from Thales Lithium Ion Cobalt Battery with Internal Contactor Flammability Analysisother
- Materials 15C – Excerpts from Thales Lithium Ion Cobalt Battery with Internal Contactor Acceptance Test Procedureother
- Materials 15E – Excerpts from Thales Li-Ion Battery System Safety Assessmentother
- Materials 15G – Excerpts from Boeing Battery Specification Control Drawingother
- Materials Laboratory - NSWCCD - XPS Investigation of Battery 412 Cell 1other
- NTSB GC Letter to Boeing GCother
- Notice of Hearing 1Eother
- Order of Hearing 1Aother
- Party Submission - Boeingother
- Party Submission - GS Yuasa Corporationother
- Party Submission - Thales Avionics Electrical Systemsother
- Safety Recommendation Letter A-14-032 thru -036other
- System Safety and Certification 18B – Table 4-2 Boeing Electrical Power System and Window Heat Control Unit Safety Assessmentother
- System Safety and Certification 18C – Table 3-1 Boeing Electrical Power System and Window Heat Control Unit Safety Assessmentother
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