What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 AND STRINGER 13L IN THE BEND RADIUS, 1.1" IN LENGTH. REPAIRED IAW EO 13-1900-53-036. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 AND STRINGER 13L IN THE BEND RADIUS, 1.1" IN LENGTH. REPAIRED IAW EO 13-1900-53-036. MAJOR REPAIR.