As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 RT ELEVATOR UPPER SKIN SURFACE I/B SIDE HAS A LIGHTENING STRIKE WITH .5 INCH CRACK STA XE 50. NDT VERIFIED .5 INCH CRACK PER NDT SPM 06-10-01.001. STOP DRILLED CRACK IAW SRM 55-2-1 FIG 10. NDT VERIFIED CRACK TERMINATES AT STOP DRILL PER NDT SPM 06-10-01.001. REPAIRED RT ELEVATOR PER SRM 55-2-1 FIG 10, CALCULATED WEIGHT/BALANCE PER SRM 51-04-08. NEW BALANCE WEIGHT IS -1445.4. INSTALLED NEW BALANCE DATA PLATE.