As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK IN WING SKIN AT NR 8 SLAT TRACK HINGED DOOR ACCESS PANEL 1289C AT WING STATION 286.6. REPAIR REQUIRED WAS OUTSIDE OF THE STANDARD SRM REPAIR SCHEME. ENGINEERING FIRM, FLIGHT VEHICLES CONSULTING PROVIDED A REPAIR SCHEME. FABRICATED, LAYED OUT NEW FASTENER PATTERN AND INSTALLED REPAIR DOUBLER IAW FVC DWG 57-12615-2.