As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 183.25 BETWEEN STRINGER 2R & 3R AT THE INBD LOWER CORNER AT AIR DUCT CUTOUT FROM A FASTENER TO THE BEND RADIUS, .2 INCHES IN LENGTH. MAJOR REPAIR, REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-025.