What was found
INSPECTION FOUND A 1.125 INCH CRACK IN MAIN CABIN DOOR JAMB INTERNAL FITTING FOR DOOR STOP. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.125 INCH CRACK IN MAIN CABIN DOOR JAMB INTERNAL FITTING FOR DOOR STOP. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-00.