As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE INTERNAL STRUCTURE UPPER LOBE DOUBLER AT BS 2517 STR 3R FOUND CRACK. STA 2517 RT SIDE CORROSION CLEARED AND CRACK STOP HOLE DRILLED. REINFORCEMENT DOUBLERS INSTALLED REF TEC-EVR-09-0002-10B STA 2517 LT SIDE, REINFORCEMENT DOUBLERS INSTALLED REF EC-EVR-09-0002-10B AND EA 53-1234. REPAIR APPROVED THROUGH 8100-9 ISSUED BY BOEING.