As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
POSSIBLE CRACK ON THE FUSELAGE UNDER THE LT TRU AFT LATCH. REMOVED AND INSTALLED NEW LH TRU AFT LATCH ANGLE REF SRM 51-42-06-001-001-A01, REO 670-53-11-2184 REV - AND DWG CC670-33040 REV -G. COMPLIED WITH ALL STEPS OF REO 670-53-11-2184 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY.