What was found
DURING OP-16, FOUND A 6 INCH CRACK IN RIGHT INBOARD FOREFLAP INBOARD RIB, AND FOUND CRACK IN ANGLE. REPAIRED BY REPLACING RIB AND ANGLE PER SRM 50-10-01 AND TWA STANDARD PRACTICES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP-16, FOUND A 6 INCH CRACK IN RIGHT INBOARD FOREFLAP INBOARD RIB, AND FOUND CRACK IN ANGLE. REPAIRED BY REPLACING RIB AND ANGLE PER SRM 50-10-01 AND TWA STANDARD PRACTICES.