As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACK ON E/E COOLING DUCT CUTOUT. LOWER FUSELAGE BS BETWEEN 360-380 AND 28L/R. ACP HFEC OF SUSPECT CRACK IN SKIN AFT OF EQUIP COOLING EXHAUST OPENING. AREA IS CRACKED APPROX ONE HALF INCH LONG FROM EXHAUST OPENING AND TERMINATED AT SCREW FASTENER HOLE. EDDY CURRENT DOES NOT INDICATE PROGRESSION BEYOND FASTENER HOLE. LAID OUT AND MFG'D SINGLE PLATE DOUBLER. ACCOMPLISHED INTERIM REPAIR PER UA-EVA-72751.