As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SKIN PULLED AWAY FROM 2 RIVETS LOWER LEFT FUSELAGE NEAR LEADING EDGE OF FORWARD WING/FUSELAGE FAIRING ATTACH ANGLE, MARKED. REMOVED STRINGER ABOVE POPPED RIVETS AND FOUND CORROSION ON STRINGER. SPLICED IN NEW SECTION OF STRINGER BETWEEN FRAMES 20 AND 21 AT ABOUT 5 O'CLOCK POSITION IAW SRM 53-00-03.