What was found
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 2.5 INCH LONG CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER OF FORWARD SERVICE DOOR CUT OUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TR 53-10-19, REV A. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 2.5 INCH LONG CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER OF FORWARD SERVICE DOOR CUT OUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TR 53-10-19, REV A. (X)