What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500 TO 510 BETWEEN STRINGER 3L AND 4L. THE DENTED AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500 TO 510 BETWEEN STRINGER 3L AND 4L. THE DENTED AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2.