What was found
AT D CHECK, CORROSION AT LT MOUNTING FLANGE FOR LOWER FUSELAGE ACCESS PANEL NR 1104 INTERIOR AND EXTERIOR. REPLACED CHORD ANGLE PER SRM 51-30-2, 52. N/R 3917.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D CHECK, CORROSION AT LT MOUNTING FLANGE FOR LOWER FUSELAGE ACCESS PANEL NR 1104 INTERIOR AND EXTERIOR. REPLACED CHORD ANGLE PER SRM 51-30-2, 52. N/R 3917.