As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H TRANSITION ANGLE HAS MULTIPLE AREAS OR CORROSION BETWEEN STA. 727F - 727I. REMOVED DAMAGE; ORIGINAL THICKNESS .045IN; REMOVED MATERIAL .007IN; REMAINING THICKNESS .038IN. FOUND TO BE OUT OF LIMIT PER SRM 53-00-53. BLENDED CORROSION REMOVED .002? MATERIAL FOUND TO BE WITHIN LIMITS PER SRM 53-00-53 1A-2;[04] C/W INSPECTION. TREATED AND PRIMED PER SRM 51-20-01.