What was found
INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR UPPER AFT OVERCENTER STOP LOCK FITTING. THE STOP LOCK, FITTING, AND PLATE WERE REMOVED. A NEW FITTING, STOP LOCK, AND PLATE WERE INSTALLED IAW SRM 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR UPPER AFT OVERCENTER STOP LOCK FITTING. THE STOP LOCK, FITTING, AND PLATE WERE REMOVED. A NEW FITTING, STOP LOCK, AND PLATE WERE INSTALLED IAW SRM 51-10-1.