What was found
FUSELAGE AT STA 840 STRINGER 21L WAS CORRODED. REMOVED DAMAGED SECTION, FABRICATED AND VERIFIED REPAIR PART, TREATED, PRIMED AND INSTALLED IN REF TO SRM 53-00-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE AT STA 840 STRINGER 21L WAS CORRODED. REMOVED DAMAGED SECTION, FABRICATED AND VERIFIED REPAIR PART, TREATED, PRIMED AND INSTALLED IN REF TO SRM 53-00-03.