What was found
INSPECTION FOUND A 1.6 INCH CRACK ON RT AND LT WING INBOARD ISLAND LOWER AFT INBOARD SPLICE ANGLE OF RIB. THE SPLICE ANGLE WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 57-22-01, FIGURE 2, 51-21-01, AND 51-33-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.6 INCH CRACK ON RT AND LT WING INBOARD ISLAND LOWER AFT INBOARD SPLICE ANGLE OF RIB. THE SPLICE ANGLE WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 57-22-01, FIGURE 2, 51-21-01, AND 51-33-01.