The emergency exit, as it is, is too small to access the interior through in full gear, unless the SCBA is doffed. And even if that is done, the Lear cabin is so small, that extricating the Co-pilot from it, would be difficult due to cockpit access restrictions from the forward cabin. Either the Gulfstream can be towed away to clear the Lear wreckage and access gained from the forward left main cabin door to then access the cockpit with much more room. Or a K12 saw would have to be used to cut the fuselage open adjacent to the emergency exit, widening that access point and another cut made that removed the fuselage ceiling above the co-pilot along with at least a partial section of the right front of the forward windscreen; if the main cabin door access was either not able to be accomplished quickly or was not enough room to access the cockpit due to damage, if it was able to be accomplished.
In this accident, the normal entry door on the left forward was blocked and unusable due to it being up against the Gulfstream fuselage, hence needing to move the Gulfstream to make any access at that point possible. Only the overwing exit on the right side was useable. The engines remained running following the accident, with one engine flaming out in about 5 or so mins, and the second one having to be drowned by water/foam to shut it down about 5-10 mins after the first one. There was no immediate access to the throttles or fuel shutoffs due to the crush destruction of the cockpit; with the resultant loss of occupiable space contributing to the fatal injuries of the pilot.
K12 saw below, being used in a vehicle extrication cutting operation we worked.
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