As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
During H-ck in Atl inspection of subject area revealed a typical crack less than 2 inches in the door corner. Repair was accomplished per sr09530117 and EA 99-185210. Section 1 provides for an alternate fastener configuration due to restricted access and structural interferance as shown on figure 1.