What was found
RIGHT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 20 INCHES OUTBOARD OF INBOARD WHEEL WELL. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PIR ER/A 540747-14 REV O AND ER/A 540747-14 ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 20 INCHES OUTBOARD OF INBOARD WHEEL WELL. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PIR ER/A 540747-14 REV O AND ER/A 540747-14 ORIGINAL.