What was found
INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD MIDFLAP RIB OUTBOARD OF INBOARD CARRIAGE SPINDLE MOUNT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-10-5, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD MIDFLAP RIB OUTBOARD OF INBOARD CARRIAGE SPINDLE MOUNT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-10-5, FIGURE 1.