What was found
DURING M CHECK, CORROSION REMOVED EXCEEDS LIMITS AT 5 FASTENER LOCATIONS ON THE FITH SLAT PRESSURE PANEL LOWER ATTACH ANGLE CAP. REPAIRED PER EA 99-169178.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING M CHECK, CORROSION REMOVED EXCEEDS LIMITS AT 5 FASTENER LOCATIONS ON THE FITH SLAT PRESSURE PANEL LOWER ATTACH ANGLE CAP. REPAIRED PER EA 99-169178.