What was found
DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1043 AND Y=1060-1068 BTW LONGERON 18-19LT REF MD88 SRM 53-04D FIG 53. FUSELAGE WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-0 4D PARA 57.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1043 AND Y=1060-1068 BTW LONGERON 18-19LT REF MD88 SRM 53-04D FIG 53. FUSELAGE WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-0 4D PARA 57.