What was found
SKIN CORROSION FOUND ON THE RIGHT SIDE OF THE FORWARD FUSELAGE BETWEEN FUSELAGE FRAMES 7 AND 9, AND BETWEEN STRINGERS 19 - 22R DURING ROUTINE INSPECTION. CORRODE MATERIAL REMOVED AND AN EXTERNAL SKIN PATCH INSTALLED RD 16-09 REV. A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SKIN CORROSION FOUND ON THE RIGHT SIDE OF THE FORWARD FUSELAGE BETWEEN FUSELAGE FRAMES 7 AND 9, AND BETWEEN STRINGERS 19 - 22R DURING ROUTINE INSPECTION. CORRODE MATERIAL REMOVED AND AN EXTERNAL SKIN PATCH INSTALLED RD 16-09 REV. A.