What was found
CORROSION TO RIGHT INBOARD FLAP 21.5 INCHES FROM INBOARD END. INSTALLED PERMANENT HOT BONDED DOUBLER AS PER SRM 51-70-10-2R 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION TO RIGHT INBOARD FLAP 21.5 INCHES FROM INBOARD END. INSTALLED PERMANENT HOT BONDED DOUBLER AS PER SRM 51-70-10-2R 4.