What was found
INSPECTION FOUND CORROSION ON FRAME LOWER CHORD AT STA 360 BETWEEN STRINGER 28L AND 28R. THE CORRODED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-10-1 AND 51-10-6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND CORROSION ON FRAME LOWER CHORD AT STA 360 BETWEEN STRINGER 28L AND 28R. THE CORRODED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-10-1 AND 51-10-6.