What was found
CORROSION BETWEEN BS 1120 - 1140, LT CHANNEL UNDER PANEL 197EL. INSTALLED A NEW STIFFENER BETWEEN BS 1120-1140 LEFT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION BETWEEN BS 1120 - 1140, LT CHANNEL UNDER PANEL 197EL. INSTALLED A NEW STIFFENER BETWEEN BS 1120-1140 LEFT.