As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT FUSELAGE SKIN STA 497 LONGERON 17L WITH DENT DAMAGE IS D=1.2", X=.034"(DEPTH) D/X DIMENSION IS 35.29 ORIGINAL SKIN THICKNESS IS 0.050" COLD FORMER SKIN PER DC9 SRM 53-04 FIG 38. PERFORMED HFEC INSP PER NDT SPM 06-10-01.001 NO CRACKS NOTED IN DENTED AREA. FABBED AND INST 1EA INTERNAL DOUBLER AND 2EA SHIMS IAW DC9 SRM 53-04 FIG 38. INSTALLED ID TAG PER PS 900-5-1 NO.04.