What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS IN THE FUSELAGE FRAME AT BS 303.25 AND STRINGER 2L, ON INBD AND OTBD SIDE OF STRINGER 2L, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-039. 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 TWO CRACKS IN THE FUSELAGE FRAME AT BS 303.25 AND STRINGER 2L, ON INBD AND OTBD SIDE OF STRINGER 2L, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-039. MAJOR REPAIR.