What was found
DURING A ROUTINE INSPECTION, CORROSION WAS NOTED AT FRAME 21, BETWEEN STRINGERS 20 AND 21R. CORROSION DAMAGE WAS REMOVED AND REPAIRED IAW SRM 53-00-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A ROUTINE INSPECTION, CORROSION WAS NOTED AT FRAME 21, BETWEEN STRINGERS 20 AND 21R. CORROSION DAMAGE WAS REMOVED AND REPAIRED IAW SRM 53-00-01.