What was found
UPPER T/E PANEL SUPPORT ANGLE IS CORRODED LOCATED FROM THE SIDE OF BODY TO #6 FLAP FITTING JUST AFT OF RMLG SUPPORT BEAM
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER T/E PANEL SUPPORT ANGLE IS CORRODED LOCATED FROM THE SIDE OF BODY TO #6 FLAP FITTING JUST AFT OF RMLG SUPPORT BEAM