What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE FUSELAGE FRAME FLANGE AT FS 183.25 AND STRINGER 2R, 1.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-047.
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 ON THE FUSELAGE FRAME FLANGE AT FS 183.25 AND STRINGER 2R, 1.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-047.