What was found
MCI - DURING C-CHECK, FOUND CRACK IN LEFT FUSELAGE FRAME AT 5TH HOLE FROME BOTTOM OF FUSELAGE FRAME. REPAIRED PER DWG NR 65C36280, SHEET 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MCI - DURING C-CHECK, FOUND CRACK IN LEFT FUSELAGE FRAME AT 5TH HOLE FROME BOTTOM OF FUSELAGE FRAME. REPAIRED PER DWG NR 65C36280, SHEET 1.