As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT TRANSITION ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES @ 727 H TO 727 I / TRANSISITON ANGLE BEING REPLACED FROM STA 727F+10 TO 787+10ON NR D389277PART# 146A7502-52ORIGINAL THICKNESS .040' : PER CORROSION SECTION W/TH NO BLEND REPAIR.