As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1084-1089 ON L29L, Y=1124-1133 BTW LONGERON 23-26L, Y=1115 BTW LONGERON 20-21L AND Y=1105 BTW LONGERON 19-20L REF MD88 SRM 53-04D FIG 53 FOR REPAIR. FUSELAGE SKIN WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-04D PARA 57.