As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND IN THE FUSELAGE AFT UPPER LT CHANNEL PN 206-031-314-145. THE CRACK IS LOCATED WHERE THE CHANNEL & THE AFT UPPER LT LONGERON ARE RIVETED TOGETHER. THE CRACK SPANS THE ENTIRE WIDTH OF THE CHANNEL. PROBABLE CAUSE IS NORMAL WEAR & TEAR.