What was found
DOOR 2 RT SILL PLATE HAS CORROSION AT CLIP NUT HOLE AT FRAME 66. REMOVED CORROSION AND INSTALLED 2 EA REPAIR ANGLES REF SRM 53-41-14 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DOOR 2 RT SILL PLATE HAS CORROSION AT CLIP NUT HOLE AT FRAME 66. REMOVED CORROSION AND INSTALLED 2 EA REPAIR ANGLES REF SRM 53-41-14 FIG 201.