As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MZJ - DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE FUSELAGE FRAME WEB, INNER AND OUTER CHORDS AT BS 148, BETWEEN STRINGERS 16R AND 18R. REPAIRED BY TRIMMING AWAY THE DAMAGED AREA PER DC9 SRM CHAPTER 53-03-32 REPAIR CONCEPT WITHOUT THE NESTED REPAIR ANGLE. REPAIRED IAW EVERGREEN INTERNATIONAL AIRLINES ECRA 915-53-026-2. (X)