What was found
FOUND CORROSION ON UPPER FLANGE C 27 RT BETWEEN OUTER STRUT AND CORNER FITTING. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CORROSION ON UPPER FLANGE C 27 RT BETWEEN OUTER STRUT AND CORNER FITTING. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.