What was found
INSPECTION FOUND A 10 INCH CRACK IN HORIZONTAL STABILIZER RIGHT I/B LEADING EDGE I/B ANGLE AT XHR 9.652. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05, 51-10-04, AND 51-30-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 10 INCH CRACK IN HORIZONTAL STABILIZER RIGHT I/B LEADING EDGE I/B ANGLE AT XHR 9.652. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05, 51-10-04, AND 51-30-01.