As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FOUND AT FASTENER HOLE AT LOWER WEB PANEL;FWD EDGE;21 3/4' FROM BOTTOM EDGE. CRACK FOUND AT FASTENER HOLE AT LOWER INNER SKINFWD EDGE21 3/4' FROM BOTTOM EDGE.<[01] ACCOMPLISHED DOUBLER REPAIR AT R1 DOOR LOWER INNER SKIN PER 24-152-02993-WIP1 AND SRM 51-40-02-0G0--0;[02] VERIFIED STEP 1;[03] ALL STEPS C/W