What was found
DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE FORWARD FUSELAGE SKIN AT FRAME 14 & STRINGER 36L. REPAIRED IAW EC A17-099-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE FORWARD FUSELAGE SKIN AT FRAME 14 & STRINGER 36L. REPAIRED IAW EC A17-099-01.