What was found
RIGHT OVERWING EXIT DOOR PAN AT UPPER AFT STOP FITTING CRACKED IN RADIUS. INSTALLED DOUBLER IAW SRM 52-05-00-001 FIGURE 51 & EA COMP-52-035000.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT OVERWING EXIT DOOR PAN AT UPPER AFT STOP FITTING CRACKED IN RADIUS. INSTALLED DOUBLER IAW SRM 52-05-00-001 FIGURE 51 & EA COMP-52-035000.