What was found
RIGHT AFT OVERWING EXIT DOOR PAN IS CRACKED AT NR 12 STOP PAD. REPAIRED WITH AN INTERNAL DOUBLER IAW SRM 52-05-00-001 FIGURE 51 SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT AFT OVERWING EXIT DOOR PAN IS CRACKED AT NR 12 STOP PAD. REPAIRED WITH AN INTERNAL DOUBLER IAW SRM 52-05-00-001 FIGURE 51 SHEET 3.