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 ON THE BS 1256 FRAME WEB AT STRINGER 26R. INTERIM REPAIR WAS ACCOMPLISHED PER SECTION I OF EA 63-208895. REPETITIVE INSPECTIONS PER SECTION II TO BE ACCOMPLISHED EVERY 2000 CYCLES. SECTION III WILL BE BASED ON SECTION II FINDINGS.