What was found
INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR FORWARD UPPER PAN AT PULLEY BRACKET ATTACH POINT. THE FRAME PAN WAS REMOVED AND REPLACED IAW SRM 51-10-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR FORWARD UPPER PAN AT PULLEY BRACKET ATTACH POINT. THE FRAME PAN WAS REMOVED AND REPLACED IAW SRM 51-10-02.