What was found
LEFT FORWARD OVERWING EXIT DOOR PAN CRACKED AT UPPER AFT CORNER. DYE CHECKED AND STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 52-05-00 FIGURE 51.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FORWARD OVERWING EXIT DOOR PAN CRACKED AT UPPER AFT CORNER. DYE CHECKED AND STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 52-05-00 FIGURE 51.