Ethiopian Airlines – Boeing B787-800 (ET-AOP) flight ET710

by | Oct 29, 2017 | Aviation Accident | 0 comments

Ethiopian Airlines flight ET710 , a Boeing B787 , landed at London Heathrow Airport at 0527 hrs on 12 July 2013 after an uneventful fight from Addis Ababa and arrived on Stand 326 at about 0540 hrs.

The fight crew did not report or record any.

After passenger and crew disembarkation, the aircraft was towed to Stand 592 to await its next service later that day. Before leaving the aircraft the engineer, on the fight deck, instructed the ground handling agent to remove ground electrical power.

The ground handling agent of Ethiopian Airlines flight ET710 accordingly turned off ground power at the stand’s control box but left the power umbilical cables attached. The engineer confirmed on the fight deck that ground power was . He then secured and left the aircraft, shortly after 0730 hrs.

At approximately 1534 hrs an employee in the air traffic control tower noticed smoke emanating from Ethiopian Airlines flight ET710 and activated the crash alarm.

The Rescue and Fire Fighting Service (RFFS) arrived on scene at 1535 hrs and discharged water and foam onto the outside of the aircraft. One fire fighter removed the power umbilical cables from the aircraft as a precaution.

Ethiopian Airlines flight ET710

Ethiopian Airlines flight ET710

Fire fighters equipped with breathing apparatus entered the aircraft at 1537 hrs via the L2 door and encountered thick smoke.

As they moved to the rear of the aircraft the smoke became denser so they opened further cabin doors to clear the smoke.

At the rear of the passenger cabin they observed indications of fire in a gap between two overhead luggage bins.

They were unable to use a hose-reel as the gap was too small and discharged a handheld ‘Halon’ extinguisher through the gap, about 20 minutes after entering the cabin.

This was ineffective, so they removed some ceiling panels to expose the area and to get better access. At this point a small amount of flame was visible.

This was extinguished with several pulses of water spray from their hose-reel, about 25 minutes after entering the cabin. A thermal-imaging camera was used to identify affected areas requiring further cooling.

The following causal factors were identified in the ground fire:

  • A thermal runaway failure of the lithium manganese dioxide battery in the ELT resulted in the uncontrolled release of stored energy within the battery cells.
  • The location and orientation of the ELT, and the compromised seal on the battery cover-plate, allowed the resulting hot gas, flames and battery decomposition products to impinge directly on the aircraft’s composite fuselage structure, providing sufficient thermal energy to initiate a fire in the rear fuselage crown.
  • The resin in the composite material provided fuel for the fire, allowing a slow-burning fire to become established in the fuselage crown, which continued to propagate from the ELT location even after the energy from the battery thermal runaway was exhausted.
  • The Navigation Radio System safety assessment conducted in support of the ELT certification did not identify any ELT battery failure modes which could represent a hazard to the aircraft and therefore these failure modes were not mitigated in the ELT design or the B787 ELT installation.

The following factors most likely contributed to the thermal runaway of the ELT battery

  • The trapped ELT battery wires created a short-circuit condition, providing a current path for an unplanned discharge of the ELT battery
  • The ELT battery may have exhibited an unbalanced discharge response, resulting in the early depletion of a single cell which experienced a voltage reversal, leading to a thermal runaway failure.
  • The Positive Temperature Coefficient protective device in the battery did not provide the level of external short-circuit protection intended in the design.
  • There was no evidence that the reset behaviour and the implications of the variable switching point of the PTC, had been fully taken into account during the design of the ELT battery.
  • The absence of cell segregation features in the battery or ELT design meant the single-cell thermal runaway failure was able to propagate rapidly to the remaining cells.


Download Report

Ethiopian Airlines – Boeing B787-800 (ET-AOP) flight ET710

Event date: 20130712
Model: B787-800
Registration: ET-AOP
msn: 34744
Location: London Heathrow, England

You may like to review this event, with a similar cause:

Summit Air – Dornier DO228-202 (C-FYEV)

The Summit Air Dornier C-FYEV (a Dornier 228-202 serial number 8133) was a charter flight from Resolute Bay to Cambridge Bay, Nunavut, under instrument flight rules. While on final approach to Runway 31 True, the aircraft collided with the ground approximately 1.5...


Submit a Comment

Your email address will not be published. Required fields are marked *