As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE HAS DENT APPROXIMATELY 4FT FWD OF OUTFLOW VLV. =1 & Y=.047 & DENT IS IN MIDDLE OF BAY NOT AFFECTING INTERNAL STRUCTURE & SMOOTH. CUT OUT DAMAGED SKIN AT BS 1585 LT, BETWEEN STRINGER 22L TO STRINGER 23L. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-01.