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X.         Ignition Source(s) and Explosions


                          Two explosions occurred almost immediately after the blowout when the
                   large gas plume that had developed over the rig came in contact with one or
                   more ignition sources on the rig.  The Panel considered the following possible
                   sources of ignition: (1) main engines and engine switch gear rooms; (2) mud gas
                   separator; (3) electrical equipment in hazardous areas; (4) friction and mechanical
                   sources; (5) non‐hazardous area sources; and (6) electrostatic discharge.

                          It is not possible to determine with certainty the source of ignition because
                   much of the physical evidence relevant to making such a determination was lost
                   with the rig or otherwise is not available.  Based upon its review of witnesses
                   testimony and other evidence, the Panel concluded that the main engines (and
                   switch gear rooms) and the mud gas separator were the most likely ignition
                   sources.

                              A.     Main Engines and Engine Switch Gear Rooms

                                   1.    Configuration of Engine Rooms on the Rig

                          The Deepwater Horizon had six engines located on the third deck of the rig.
                   Each engine was in an engine room that was equipped with air intake systems.
                   Each air intake system drew air from vents located in the engine room in which it
                   sat.  Each engine room had an engine switch gear room attached to it.

                          The Deepwater Horizon’s engine rooms and switch gear rooms were
                   located in “unclassified” areas, which were areas that did not require explosion‐
                   proof enclosures, intrinsically‐safe equipment, and/or purged and pressurized
                   equipment.  The engines and switch gears in the non‐classified areas were not
                   designed or tested to ensure that they would not initiate an explosion.

                          The engines had multiple redundant safety systems and shutdown

                   devices designed to shut down the engines in an over‐speed situation.  Engine
                   over‐speed is a condition where an engine’s revolutions per minute (“rpms”)
                   exceed their normal operating speed.  This condition can occur when
                   combustible gas is drawn into the intake system.  To prevent this, the air intake
                   systems included a shut‐off device (sometimes referred to as a “rig saver”) that








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