What was found
DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE CHANNEL AT BS 177.35, IN THE BEND RADIUS AT THE OTBD END OF THE CHANNEL, 1.2 INCH IN LENGTH. REPAIRED IAW EO 15-1900-53-002. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE CHANNEL AT BS 177.35, IN THE BEND RADIUS AT THE OTBD END OF THE CHANNEL, 1.2 INCH IN LENGTH. REPAIRED IAW EO 15-1900-53-002. MAJOR REPAIR.