As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED A CRACK IN FUSELAGE SKIN AT UPPER HINGE CUT-OUT AT FORWARD ENTRY DOOR. TRIMMED DAMAGED AREA PER SB 727-53-0198. FABRICATED AND INSTALLED DOUBLER PER SB 727-53-0198. TT: 65,345:17 HOURS. TC: 43,816. (X)