What was found
DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FUSELAGE FRAME AT BS 183.25, BETWEEN STRINGERS 2 & 3R. CRACK RADIATES DOWNWARD FROM FASTENER, .2 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-027. MAJOR REPAIR .
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FUSELAGE FRAME AT BS 183.25, BETWEEN STRINGERS 2 & 3R. CRACK RADIATES DOWNWARD FROM FASTENER, .2 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-027. MAJOR REPAIR .