As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION (MID-FEC) FOUND CRACK INDICATION AT FRAME BS 380 R BETWEEN STRINGERS 8 & 9 AT AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO FUSELAGE FRAME MARKED. PER EA 5310-04716 REV E OPT 1. INSTALLED REPAIR AT BS 380 R BETWEEN STRINGERS 8 & 9 PER EA 5310-04716 REV E. SEE ENTRIES BELOW FOR ALL WORK ACCOMPLISHED.