What was found
INSPECTION FOUND A .25 INCH CRACK IN HINGE FITTING FORWARD OF OUTBOARD AILERON, SECOND HINGE FROM OUTBOARD END. THE HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN HINGE FITTING FORWARD OF OUTBOARD AILERON, SECOND HINGE FROM OUTBOARD END. THE HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.