What was found
CRACK FOUND IN DORSAL FIN SKIN AFT OF WRAP AROUND ACCESS PANEL. STOP DRILLED CRACK & INSTALLED DOUBLER IAW SRM 555-01-00 FIGURE 2 SHEET 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND IN DORSAL FIN SKIN AFT OF WRAP AROUND ACCESS PANEL. STOP DRILLED CRACK & INSTALLED DOUBLER IAW SRM 555-01-00 FIGURE 2 SHEET 2.