As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AD 2009-01-02 BETWEEN STRINGER 8L & 9L AT THE AIR CONDITIONING OUTLET EXTRUSION, SUPPORT ATTACHMENT TO THE FUSELAGE FRAME FOUND CRACK AT STATION 500C LT ON MFEC IAW EA 5310-04716 REV F OP 1. FRAME 500C LT HAS BEEN REPAIRED IAW EA 5310-04716 REV F OP 1.