What was found
FRAME 23 BETWEEN STRINGERS 20L AND 20R IS CORRODING OUTBOARD OF STRINGER 21L, DISCOVERED AT C-CHECK. COMPLIED WITH REPAIR OF FUSELAGE SKIN AT FRAME 23 BETWEEN STRINGERS 20L AND 20R PER EMBRAER APPROVED REPAIR #1C2007-120/03354.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME 23 BETWEEN STRINGERS 20L AND 20R IS CORRODING OUTBOARD OF STRINGER 21L, DISCOVERED AT C-CHECK. COMPLIED WITH REPAIR OF FUSELAGE SKIN AT FRAME 23 BETWEEN STRINGERS 20L AND 20R PER EMBRAER APPROVED REPAIR #1C2007-120/03354.