As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 2.5 INCH CRACK IN LT ELEVATOR O/B TRAILING EDGE SKIN (JUST I/B OF STATIC WICK). THE CRACK WAS STOP DRILLED AND A FIBERGLASS REPAIR WAS INSTALLED IAW SRM 51-70-1, PAGE 12. WEIGHT AND BALANCE WAS WITHIN LIMITS IAW SRM 55-20-1, FIGURE 4.