As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ICT - OVERNIGHT MAINTENANCE INSPECTION FOUND LEFT INBOARD FLAP DOVETAIL CRACKED. STOP DRILLED CRACK WITH A NR 45 DRILL BIT. FABRICATED 4 INCH BY 2 INCH PATCH OUT OF DOVE TAIL SKIN STOCK. PLACED PATCH OVER CRACKS. ALL WORK DONE USING SRM'S 51-00, 51-30, 51-40, AND T.O. 1900-27-00-0001. (X)