What was found
INSPECTION FOUND A .5 INCH CRACK JUST BELOW UPPER HINGE, LOWER GUIDE PLATE AREA IN R-1 DOOR FUSELAGE CUTOUT FRAME, STA 294.5, S11 R TO S14R. THE DOOR FUSELAGE CUTOUT FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK JUST BELOW UPPER HINGE, LOWER GUIDE PLATE AREA IN R-1 DOOR FUSELAGE CUTOUT FRAME, STA 294.5, S11 R TO S14R. THE DOOR FUSELAGE CUTOUT FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.