English: The left-side fuselage skin exhibited thermal damage (missing and charred paint) from just aft of the 2L door to just past the wing leading edge, and the center of this thermally damaged area exhibited buckling and cracks in the skin, the longest of which was about 12 inches. The cracks in the skin coincided with the area of most severe thermal damage to the wall panels in the interior of the airplane. The wing-to-body fairings on the left side of the airplane exhibited widespread delamination and blistering. The skin on the composite fairing at the wing/fuselage interface was completely delaminated, and the skin aft of the interface for the underwing and overwing fairings was blistered. The composite panels near the wing-to-body junction were thermally damaged and delaminated. The wing-to-body fairing panels on the right side of the airplane also sustained thermal damage and exhibited delamination but to a lesser degree than that on the left side.