English: Thermal damage on the exterior of the airplane was concentrated along its midsection, from the left engine to the right side of the fuselage. On the left engine, the cowling was thermally damaged from the 4:00 to 12:00 positions (as viewed from the front of the engine). The thermal damage between the 6:00 and 12:00 positions (the inboard side of the left engine, as shown in figure 2 [inboard side of left engine]) caused the composite cowling to delaminate and the aluminum leading edge of the cowling to partially melt along the 7:00 to 8:00 positions. The interior of the left engine had soot on some surfaces but no significant thermal degradation to the components. The left wing sustained thermal damage in the area between the left engine and the fuselage. No evidence indicated engine debris impacting or penetrating the left wing structure. The top and bottom wing surfaces that were outboard of the strut did not exhibit any damage from the fire.