As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BETWEEN STRINGER 8 & STRINGER 9 AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME, FOUND CRACK AT STATION 500C RT. REPAIRED CRACK IN FRAME AT STATION 500C BETWEEN STRINGER 8R & STRINGER 9R IAW EA 5310-04716 REV F OP 1.