What was found
CORROSION DAMAGE TO THE UPPER FLANGE OF THE FRAME 17 CROSSBEAM. THE DAMAGE WAS BLENDED, THE DAMAGE IN THE CENTER OF THE BLEND OUT EXTENDED THROUGH THE ENTIRE THICKNESS OF THE UPPER FLANGE. REPAIRED IAW ETD2016-170-081507A, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION DAMAGE TO THE UPPER FLANGE OF THE FRAME 17 CROSSBEAM. THE DAMAGE WAS BLENDED, THE DAMAGE IN THE CENTER OF THE BLEND OUT EXTENDED THROUGH THE ENTIRE THICKNESS OF THE UPPER FLANGE. REPAIRED IAW ETD2016-170-081507A, FIGURE 1.