What was found
INSPECTION FOUND A 0.6 CRACK IN FITTING AT RT INBOARD MIDFLAP RIB LEADING EDGE JUST OUTBOARD OF NR 5 CARRIAGE. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4. FASTENERS WERE INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.6 CRACK IN FITTING AT RT INBOARD MIDFLAP RIB LEADING EDGE JUST OUTBOARD OF NR 5 CARRIAGE. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4. FASTENERS WERE INSTALLED IAW SRM 51-30-2.