As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PUNCTURE IN THE UPPER SKIN OF SPOILER, APPROX 25.5 FROM O/B EDGE, 4 INCHES FROM TRAILING EDGE. REPAIR CONSISTED OF BONDING 3 REPAIR PLIES USING GRAPHITE CLOTH REPAIR MATERIAL AND 9390 ADHESIVE RESKIN SYSTEM, CURED AT 200 DEGREES FOR A TOTAL OF FOUR HOURS AS CALLED OUT IN THE 57-70-01 REF 51-70-17.