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 867R BETWEEN STRINGERS 8 & 9 AT AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO FUSELAGE FRAME. PER EA 5310-04716 REV E OPT 1. CUT DAMAGED AREA OF FRAME, FABRICATED & INSTALLED REPAIR ANGLES REFERENCE EA 5310-04716 REV E.