What was found
DURING A SCHEDULED INSPECTION FOUND CRACK IN THE LT AFT FUSELAGE SKIN AT BS 549.25 BETWEEN STRINGERS 12 - 13L, 1.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-043. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED INSPECTION FOUND CRACK IN THE LT AFT FUSELAGE SKIN AT BS 549.25 BETWEEN STRINGERS 12 - 13L, 1.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-043. MAJOR REPAIR.