What was found
AT C-CHECK, INBOARD MID FLAP TRAILING EDGE ANGLE IS CRACKED AT CUT OUT FOR INBOARD ACTUATING ROD. REMOVED SKIN PANEL, STOP DRILLED CRACK, INSTALLED ANGLE REPAIR PER SRM 51-40-4, 12 BY 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, INBOARD MID FLAP TRAILING EDGE ANGLE IS CRACKED AT CUT OUT FOR INBOARD ACTUATING ROD. REMOVED SKIN PANEL, STOP DRILLED CRACK, INSTALLED ANGLE REPAIR PER SRM 51-40-4, 12 BY 2.