As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE B-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 242, BETWEEN LONGERONS 28L AND 29L. REPAIR ACCOMPLISHED STOP DRILLING CRACK. FABRICATION AND INSTALLATION A REPAIR DOUBLER IN ACCORDANCE WITH DACO STRUCTURAL REPAIR MANUAL 51-1-20 AND 53-2-0.