What was found
INSPECTION FOUND STRINGER 26L CORRODED UNDER TRANSITION PANEL AT STA 500A TO 500B. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND STRINGER 26L CORRODED UNDER TRANSITION PANEL AT STA 500A TO 500B. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201.