As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 .375 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE LOWER AFT CORNER OF L-1 DOOR, BS 344. MAINTENANCE CUTOUT DAMAGE ON FUSELAGE SKIN AT LOWER AFT CORNER OF L-1 DOOR; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS AND 2 EACH REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW ER 15-5300-03311-TB2.