As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO CRACKS AT LEADING EDGE ACCESS PANEL NR 2 OF RUDDER INNER SKIN, HONEYCOMP CORE AND OUTER SKIN CRACKED AT ACCESS HOLE EDGES, MAX CRACK LENGTH = 75MM. REPAIR PERFORMED BY WET-LAY-UP REPAIR AS PER TD/K4/S1/19611/2005/A, APPROVED BY EA 6-5542-82890 AND RAS/DAHAM/4019611/2005 ISSUE A.