What was found
CRACK PANEL RUDDER REAR CENTER SPAR TO REAR SPAR LWR PANEL RT SIDE. REPAIRED THE CRACK AREA IAW MD11 SRM 55-30-02 FIG 201 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK PANEL RUDDER REAR CENTER SPAR TO REAR SPAR LWR PANEL RT SIDE. REPAIRED THE CRACK AREA IAW MD11 SRM 55-30-02 FIG 201 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.