As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING "M" CHECK, FOUND CRACK IN FRAME WEB HOLE AT BS 1265 S26L. ACCOMPLISHED INTERIM REPAIR PER EA 63-208916 SECTION I. REPETITIVE INSPECTIONS TO BE ACCOMPLISHED PER SECT II EVERY 2000 CYCLES. SECTION III PERMANENT REPAIR TO BE ACCOMPLISHED BASED ON SECTION II INSPECTION FINDINGS.